AIAA / SAE / NASA Technical Papers
Barnhart, Billy P. and Ratvasky, Thomas P.: Effective Training for Flight in Icing Conditions, NASA/TM -- 2007-214693, I/ITSEC 2006 Paper No. 2973, December 4-7, 2006, Orlando, Florida, US.
Barnhart, Billy P., Dickes, Edward G., Gingras, David R., Ratvasky, Thomas P.:
Simulation Model Development for Icing Effects Flight Training, SAE 2002-01-1527, SAE 2002 General Aviation Technology Conference and Exhibition, April 16-18, 2002, Wichita, Kansas.
Hultberg, Randy, Gingras, David and Bell, Jeffery: Applications of a Simulation Environment During
Wind Tunnel Testing, AIAA 2001-4423, AIAA Modeling and Simulation Technologies Conference and Exhibit, August 6-9, 2001, Montreal,
Quebec, Canada.
Gingras, David, Player, Jennifer and Blake, William: Static and Dynamic Wind Tunnel Testing of Air
Vehicles in Close Proximity, AIAA 2001-4137, AIAA Atmospheric Flight Mechanics Conference, August 6-9, 2001, Montreal, Quebec,
Canada.
Dickes, Edward, Ralston, John and Lawson, Kenneth: Application of Large-Angle Data for Flight
Simulation, AIAA 2000-4584, AIAA Modeling and Simulation Conference and Exhibit, August 14-17, 2000, Denver, CO.
Kay, Jacob and Ralston, John: Forebody Aerodynamic Asymmetry on a Full-Scale F-15 Radome, AIAA
2000-4104, AIAA Atmospheric Flight Mechanics Conference, August 14-17, 2000, Denver, CO.
Kay, Jacob: Acquiring and Modeling Unsteady Aerodynamic Characteristics, AIAA 2000-3907, AIAA
Atmospheric Flight Mechanics Conference, August 14-17, 2000, Denver, CO.
Gingras, David: AV-8B II+ Device S2F176 Flight Model Development Using A PC-Based Simulation
Environment, AIAA 99-4191, AIAA Modeling and Simulation Conference and Exhibit August 9-11, 1999, Portland, Oregon.
Gingras, David: Experimental Investigation of a Multi-Aircraft Formation, AIAA 99-3143, 17th
Applied Aerodynamics Conference June 28-July 01, 1999, Norfolk, VA.
Kay, Jacob, Ralston, John N. and Lash, Stanley: Development of Non-Linear, Low-Speed Aerodynamic Model
for the F-16/VISTA, AIAA 97-3576, AIAA Modeling and Simulation Technologies Conference, August 11-13, 1997, New Orleans, LA.
Bell, Jeffery, and O’Rourke, Matthew: Application of a Multipurpose Simulation Design, AIAA
97-3798, AIAA Modeling and Simulation Technologies Conference, August 11-13, 1997, New Orleans, LA.
O’Rourke, Matthew, Ralston, John, Bell, Jeffery, and Lash, Stanley: PC-Based Simulation of the
F-16/MATV, AIAA 97-3728, AIAA Modeling and Simulation Technologies Conference, August 11-13, 1997, New Orleans, LA.
Hultberg, Randy: Acquisition Technique and Analysis Format for Forced Oscillation Dynamic Data, NASA High Angle-of-Attack Technology
Conference, September 17-19, 1996, NASA Langley Research Center, Hampton, VA.
O’Rourke, Matthew and Ralston, John: Yaw Controls on Chined Forebodies, NASA High Angle-of-Attack Technology Conference,
September 17-19, 1996, NASA Langley Research Center, Hampton, VA.
Ralston, John and Kay, Jacob: The Utilization of High Fidelity Simulation in the Support of High-Angle-of-Attack Flight Testing, NASA
High Angle-of- Attack Technology Conference, September 17-19, 1996, NASA Langley Research Center, Hampton, VA.
Jaramillo, Paul: Flight Test Analysis
and Simulation of the F-18D Falling Leaf Motion, AIAA 96-3371, AIAA
Atmospheric Flight Mechanics Conference, July 29-31, 1996, San Diego,
CA.
Jaramillo, Paul: An Analysis of Falling
Leaf Suppression Strategies for the F/A-18D, AIAA 96-3370, AIAA
Atmospheric Flight Mechanics Conference, July 29-31, 1996, San Diego,
CA.
O’Connor, Cornelius, Ralston, John and Fitzgerald, Timothy: Evaluation of the NAWC/AD F/A-18C/D
Simulation Including Database Coverage and Dynamic Data Implementation Techniques, AIAA 96-3365, AIAA Atmospheric Flight Mechanics
Conference, July 29-31, 1996, San Diego, CA.
Ralston, John and Kay, Jacob: The Utilization of High Fidelity Simulation in the Support of High Angle
of Attack Flight Testing, AIAA 96-3354, Second Test and Evaluation International Aerospace Forum, June 25-27, 1996, London,
England.
O’Rourke, Matthew, Ralston, Jack, Kloc, Stefan and Langan, Kevin: Development of a Conformal
Pneumatic Forebody Control for Next-Generation Fighters, AIAA 96-0786, AIAA 34th Aerospace Sciences Meeting and Exhibit, January
15-18, 1996, Reno, NV.
Ralston, John: Examination of Vortex Control on a Chined Forebody During Maneuvering Flight Conditions, Fourth NASA High Alpha
Conference, July 12-14, 1994, NASA Dryden Flight Research Center, Edwards, California.
Dickes, Edward, Kay, Jacob and Ralston, John: Validation of the NASA Dryden X-31 Simulation and Evaluation of Mechanization
Techniques, Fourth NASA High Alpha Conference, July 12-14, 1994, NASA Dryden Flight Research Center, Edwards, California.
Bihrle, William Jr.: Techniques for Tailoring Aircraft Stall and Post-Stall Behavior, 1993 SAE General, Corporate, & Regional
Aviation Meeting & Exposition, May 1993, Wichita, Kansas.
Ralston, John and Barnhart, Billy: Application of Rotary Balance Data in the Analysis of High Angle-of-Attack Characteristics, NASA High
Angle-of-Attack Technology Conference, October 30 - November 1, 1990, NASA Langley Research Center, Hampton, VA.
Martin, Colin A., Hultberg, Randy S., Bowman, James S. Jr., Drobik Jan S.; Gage, Peter J.: Measurements of Pressures on the Wing of an
Aircraft Model During Steady Rotation, AIAA-90-2842, AIAA Atmospheric Flight Mechanics Conference, August 20-22, 1990, Portland,
Oregon.
Blake, William B. and Barnhart, Billy: Yaw Damping of Elliptic Bodies at High Angles of Attack, Journal of Aircraft, Vol. 27, No. 7,
July 1990.
Hultberg, Randy S., Bowman, James S. Jr., and Martin, Colin A.: Measurements of Pressures on the Tail and Aft Fuselage of an Airplane
Model During Rotary Motions at Spin Attitudes, AIAA 88-4338-CP, AIAA Atmospheric Flight Mechanics Conference, August 15-17, 1988,
Minneapolis, MN.
Ralston, J.N.: Influence of Airplane Components on Rotational Aerodynamic Data for a Typical Single-Engine Airplane, AIAA-83-2135,
AIAA Atmospheric Flight Mechanics Conference, August 15-17, 1983, Gatlinburg, Tennessee.
Bihrle, William Jr. and Barnhart, Billy: Spin Prediction Techniques, Journal of Aircraft, Vol. 20, No. 2, February 1983.
Bihrle, W. Jr. and Barnhart, B.: Departure Susceptibility and Uncoordinated Roll-Reversal Boundaries for Fighter Configurations,
Journal of Aircraft, Vol. 19, No. 11, November 1982.
Bihrle, W. Jr. and Bowman, J.S. Jr.: Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift,
Journal of Aircraft, Vol. 18, No. 11, November 1981.
Bihrle, William Jr.: Prediction of High Alpha Flight Characteristics Utilizing Rotary Balance Data, 13th ICAS Congress/AIAA Aircraft
Systems and Technology Conference Proceedings, August 1981.
Industry Technical Reports
Dickes, Edward: Wind Tunnel Investigation for the F/A-18E/F at High
Angle of Attack and Large Sideslip in the Old Dominion Langley Full-Scale
Tunnel, Test Entry #77, Bihrle 01-13, October 2001.
Hultberg, Randy S.: High Angle of Attack and Large Sideslip static
Wind Tunnel Test Results for the F/A-18C/D in the Old Dominion Langley
Full-Scale Tunnel, Test Entry #76, Bihrle 01-12, October 2001.
Hultberg, Randy S., Ralston, John N., Kay, Jacob, Kloc Stefan J., and
Stowe, Everett: Static and Dynamic Wind Tunnel Test Data and Analysis
of the F-16 Block 60, Conformal Fuel Tank, and CAT I Configurations,
Bihrle 01-09, August 2001.
Dickes, Edward: Test Plan for the Flying Qualities Low-Speed Wind Tunnel
LEX Vents Closed and Inverted Testing on the F/A-18E/F Aircraft in the
Langley Full-Scale Tunnel, Bihrle 01-08, July 2001.
Kay, J. Low-Speed Testing and Simulation Modeling for Powered Configurations:
Phase-I Report, Bihrle01-06, April 2001.
Gingras, D.R. NAWCTSD AV-8B Flight Model Update: Results, Analysis,
and Phase II Recommendations, Bihrle01-05, April 2001.
Gingras, D.R. NAWCTSD AV-8B Flight Model Update: Model Implementation
and Verification, Bihrle01-04, February 2001.
Gingras,D.R. NAVAIR AV-8B Flight Model Update, Bihrle01-03, January 2001.
Gingras, D. Kay, J., Ralston, J. NAVAIR AV-8B Validation Data Report,
Bihrle 00-2, January 2001.
Player, J. L.: F/A-18C Formation Flight Incremental Effects Simulation
Model, Bihrle 01-01, January 2001.
Eanes, J. and Gingras D., D-Six IOD Module Extension: SBS Model 616/673
VME to PCI Shared Memory Boards for use with an SCT CLoad 3.0e Force
Loader, Bihrle 00-12, February 2000.
Player, Jennifer L.: SBIR AF 00-282 Phase I Final Report: A single
Software Application for the comprehensive analysis of UCAV Stability
and Control Characteristics and Flying Qualities, Bihrle 00-11, December
2000.
Gingras, D., Kay, J.,Ralston, J.: US AV-8B Trainer Flight Model Evaluation:
Flying Qualities and Performance Criteria Data, Bihrle 00-10, November
2000.
Gingras, David.R.: US AV-8B Trainer Flight Model: Evaluation Test Plan,
Bihrle 00-09, November 2000.
Hultberg, Randy S., Kloc, Stefan J., BarnHart, Billy P.: Effects of
LEX Vent on Dynamic Damping for F-18E, Bihrle 00-07, May 2000.
Hultberg, Randy S. and Player, Jennifer: Analysis of Boeing Joined
Wing Configuration Static and Dynamic Data (Phase II SBIR N98-018 Part
III), Bihrle 00-06, May 2000.
Kay, J.: Dynamic Wind Tunnel Testing & Modeling of Nonlinear Unsteady
Aerodynamics, Phase-II Final Report, Bihrle 00-05, March 2000.
Eanes, J and Gingras, D, SBS Module document Bihrle 00-04.
Hultberg, Randy S. and Player, Jennifer: Improved Wind Tunnel Test
Technique for Measuring Dynamic Data, NAVY SBIR N96-018 Phase II, Bihrle
00-01, January 2000.
O'Connor, Cornelius J.: Analysis of Boeing JSF Static and Dynamic Wind
Tunnel Test Data and Predicted Spin Modes, Bihrle 99-09, July 1999.
Dickes, Edward: Analysis of Static and Rotary Balance Wind Tunnel Test
Data of the KTX-2 C505B+ Advanced Trainer Aircraft, Bihrle 99-08, July
1999.
Kay, Jacob: F-18E/F FEB98AERO Model Rehost Static Check Case Verification
Results, Bihrle 99-07M, July 1999.
Player, J.L., Gingras, D.R., and Ralston, J.N.: An Improved F/A-18C/D
Power Approach Aerodynamics Model, Bihrle 99-06, June 1999.
Dickes, Edward, Ralston, John and Kloc, Stefan: F18E Large-Angle Testing:
Static and Dynamic Characteristics From Rotary Balance Wind Tunnel Test
Data and Aeromodel Increments, Bihrle 99-05, June 1999.
Ralston, John; Eanes, Josh: Application of a Network Design for High-fidelity
UCAV Simulation Workstation, Bihrle99-4, April 1999.
O'Connor, Cornelius J.: Aeromodel Increments of F-18C Body-Axis Damping
Data Obtained During Forced Oscillation Wind Tunnel Tests, Bihrle 99-3M,
April 1999.
Kay, Jacob: Dynamic Data Implementation Techniques, Bihrle99-2M, March
1999.
Dickes, Edward: Analysis of Static and Rotary Balance Wind Tunnel Test
Data of a 1/10-Scale Model of the KTX-2 C504 Advanced Trainer Aircraft,
Phase II Test, Bihrle 99-01, January 1999.
Gingras, David. R., Player J., and Ralston J.N. SBIR AF98-175 PHASE
I Final Report: A Comprehensive Approach for the Development and Implementation
of Multi-Vehicle Aerodynamics Simulation Models, Bihrle 98-15, December
1998.
Dickes, Edward: Analysis of Dynamic Characteristics From Rotary Balance
And Forced Oscillation Wind Tunnel Test Data For The NASA/AFRL X-38,
Vehicle 201 From -90? TO +135? Angle Of Attack, Bihrle 98-14, November
1998.
Kay, Jacob; Bell, Jeff and Eanes, Josh: Development of PC-Based D-Six
Simulation Workstation with Piloted Capabilities. Bihrle 98-13, October,
1998.
O'Connor, Cornelius J.: F-18C Body-Axis Damping Data Obtained During
Forced Oscillation Wind Tunnel Tests, Bihrle 98-12, September 1998.
Dickes, Edward: Analysis of Static and Rotary Balance Wind Tunnel Test
Data of a 1/10-Scale Model of the KTX-2 C504 Advanced Trainer Aircraft,
Bihrle 98-11, August 1998.
Houlden, Heather P.: Analysis of Rotary Balance Wind Tunnel Test Data
for the Boeing JSF CTOL/CV (X-32A) Configuration and Steady-State Spin
Predictions - Phase II, Bihrle 98-10, July 1998.
Gingras, Dave, O'Connor, Cornelius J.: S2F176 AERODYNAMICS MATH MODEL
REPORT: Initial Delivery, Bihrle 98-9, July 1998.
Dickes, Edward: Math Modeling Techniques For Use With Dynamic Data
In X-35A/B Aircraft Simulation, Bihrle 98-8, June 1998.
AV-8B II+ Device S2F176 Trainer Criteria Report, (flying qualities
sections only), Bihrle 98-7, May 1998.
Hultberg, Randy S.: Multi-Axis Test Rig For the AFRL Vertical Wind
Tunnel, SBIR Phase II Final Report, Bihrle 98-6, May 1998.
Houlden, Heather P.: Analysis of Rotary Balance Wind Tunnel Test Data
for the Boeing JSF CTOL/CV (X-32A) Configuration and Steady-State Spin
Predictions - Phase II, Bihrle 98-4, March 1998.
Dickes, Edward: An Incremental Aerodynamic Math Model of the Lockheed
Martin JSF X-35A/B From -90° TO +90° Angle of Attack Representing
Dynamic Effects, Bihrle 98-3, March 1998.
Kay, Jacob, Hultberg, Randy, Houlden, Heather, and Ralston, John: F-18E
Body-Axis Damping Data Obtained During Forced Oscillation Wind Tunnel
Tests, Part 1: Test Results, Bihrle 98-2, February 1998.
Gingras, David. Implementation of Aircraft Asymmetry Effects in the
NAWCAD F/A-18CD Aerodynamics Model, Bihrle 98-1, February 1998.
O'Rourke, Matthew, Kay, Jacob, and Ralston, John: Implementation of
WL F-16/MATV Flight Control System Model with Non-Linear F-16/VISTA
Aerodynamic Model, Including Flight Correlation, Bihrle 97-11, October
1997.
Houlden, Heather P.: Analysis of Rotary Balance Wind Tunnel Test Data
for the Boeing JSF CTOL/CV (X-32A) Configuration and Steady-State Spin
Predictions - Phase I, Bihrle 97-10, November 1997.
Houlden, Heather P.: Low-Speed Aerodynamic Model of the Boeing JSF
CTOL/CV from -90° to +90° Angle of Attack, Bihrle 97-10M, November
1997.
Gingras, David: Full-Scale Wind-Tunnel Testing of a Chevrolet Monte
Carlo SS Racing Configuration, Bihrle 97-9M, October 1997.
Kay, Jacob and Ralston, John: F-18E/F Aerodynamic Model Issues (OCT96AERO)September
1997., Bihrle 97-8M.
Kay, Jacob and Ralston, John: F-18E RPV Flight Test & Instrumentation
Issues/Observations, Bihrle 97-7M, July 1997.
Kay, Jacob, Ralston, John, Hultberg, Randy, and Houlden, Heather: F-18E
Body-Axis Damping Data Obtained During Forced Oscillation Wind Tunnel
Tests, Part 2: Mechanization of Nonlinear Forced Oscillation Data. Bihrle
97-5, Aug. 1997.
Kay, Jacob, Kloc, Stefan and Stowe, Everett: High Angle of Attack Full-Scale
F-15 Forebody Wind Tunnel Testing. Bihrle 97-4, June 1997.
O'Connor, Cornelius: Rotary Balance Data and Analysis of the F/A-18
C/D at High Sideslip Angles, Bihrle 97-3, April 1997.
Houlden, Heather, Hultberg, Randy: F-18E Body-Axis Damping Data Obtained
During Forced Oscillation Wind Tunnel Tests, Part 1: Test Results, Bihrle
97-2, April 1997.
Dickes, Edward: Analysis of Rotary Balance and Forced Oscillation Tests
of a 1/10-Scale Model of the KTX-2 (501) Trainer Aircraft, Bihrle 96-12,
December 1996.
Hultberg, Randy, Houlden, Heather, Jaramillo, Paul: Improved Wind-Tunnel
Test Technique, Bihrle 96-11, December 1996.
Hultberg, Randy, Houlden, Heather, Kloc, Stefan: Analysis of F-18E
Forced Oscillation Dynamic Data and Acquisition Techniques During Low
Body Axis Rates, Bihrle 96-10, September 1996.
Houlden, Heather: Rotary Balance Wind Tunnel Test Investigation of
Innovative Control Effectors on Two Tailless Fighter Configurations,
Bihrle 96-9, October 1996.
O'Connor, Cornelius: Unification of the F/A-18 C/D Supersonic Update
Tables, Bihrle 96-8, October 1996.
Kay, Jacob, Hultberg, Randy and Ralston, John: Dynamic Testing and
High Fidelity Modeling of Nonlinear Unsteady Aerodynamics, Bihrle 96-7,
September 1996.
Houlden, Heather: Three-Dimensional Aerodynamic Analysis of the F/A-18E
Remotely Piloted Vehicle Using PMARC, Bihrle 96-6, August 1996.
Volume I.- Analysis Report, Volume II.- Static and Rotational Aerodynamic
Data, Bihrle 96-5, July 1996.
Ralston, John and Kay, Jacob: Development of a Large Angle Non-linear,
Low Speed Database for the F-16/VISTA, Including Correlation with Flight,
Bihrle 96-4, May 1996.
Dickes, Edward: Analysis of the High Angle of Attack Aerodynamics and
Spins for the Lockheed Martin JAST 200 Aircraft From +90? to -90? Angle
of Attack, Bihrle 96-3, April 1996.
O'Rourke, Matthew, Ralston, Jack and Kloc, Stefan: Development of a
Conformal Vortex Controller for Chined Forebody Military Aircraft, WL-TR-95-3103,
Bihrle 96-1, February 1996.
Dickes, Edward and O'Connor, Cornelius: Aerodynamic Math Model of the
KTX-2 (405) Trainer Aircraft for Simulation of Flight Motions From -90?
to +90? Angle of Attack, Bihrle 95-12, December 1995.
Dickes, Edward: Analysis of Rotary Balance and Forced Oscillation Tests
of a 1/10-Scale Model of the KTX-2 (405) Trainer Aircraft From +90?
to -90? Angle of Attack, Including Predicted Spin Modes and Calculated
Dynamic Derivatives, Bihrle 95-11, December 1995.
Houlden, Heather P.: Analysis of F-18E/F Rotary Balance Force and Moment
and Surface Pressure Data, Bihrle 95-10, November 1995.
Jaramillo, Paul and Ralston, John: Simulation and Analysis of the F/A-18D
Falling Leaf Motion with an Assessment of Suppression Strategies, Bihrle
95-9, December 1995.
Dickes, Edward: Analysis of Rotary Balance and Forced Oscillation Tests
of a 1/10-Scale Model of the KTX-2 Trainer Aircraft, Including Predicted
Spin Modes and Calculated Dynamic Derivatives Configuration 104B.WT,
Phase II Test Results, Bihrle 95-8, July 1995.
Dickes, Edward: Rotary Balance Data and Analysis of the KTX-2 Trainer
Aircraft Configuration 104B.WT, Phase I Test Results, Bihrle 95-7, April
1995.
Dickes, Edward and Hultberg, Randy: Rotary Balance Data and Predicted
Spin Modes for the KTX-1 Aircraft, Bihrle 95-6, May 1995.
Bell, Jeffery and Kay, Jacob: D-SIX, a Flight Simulation Development,
Analysis and Validation Environment, Bihrle 95-4, April 1995.
Ralston, John, O'Connor, Cornelius, Fitzgerald, Timothy and Avent,
John: Evaluation of the NAWC/AD F/A-18 C/D Simulation Including Data
Base Coverage and Dynamic Data Implementation Techniques, Volume I:
Report and Analysis, Volume II: Additional Simulation Correlation Examples,
Bihrle 95-3, December 1995.
Kay, Jacob and Ralston, John: F-15E High Angle of Attack Study, Including
Data, Analysis, Aerodynamic Math Modeling and Simulation, Bihrle 95-2,
March 1995.
Ralston, John and Dickes, Edward: Application of Dynamic Data in Aircraft
Simulation, Bihrle 95-1, January 1995.
Pauley, Heather, Ralston, John and Dickes, Edward: Experimental Study
of the Effects of Reynolds Number on High Angle of Attack Aerodynamic
Characteristics of Forebodies During Rotary Motion, Bihrle 94-4, January
1995.
O'Connor, Cornelius: Rotary Balance Data and Simulation Analysis of
the Inverted T-45 Simulation Including Large Sideslip Data, Bihrle 94-3,
October 1994.
Dickes, Edward and Ralston, John: Preliminary Design of a Test Rig
for the Wright Laboratory's Vertical Wind Tunnel, Bihrle 94-1, January
1994.
Dickes, Edward, Kay, Jacob, and Ralston, John: Validation of the NASA
Dryden X-31 Simulation Aerodynamic Math Model and Evaluation of Mechanization
Techniques, Bihrle 93-4, June 1993.
Ralston, John, Dickes, Edward, and Avent, John: A Feasibility Study
of Forebody Vortex Control on a Chined Forebody Configuration, Bihrle 93-1,
January 1993.
Hultberg, Randy: Documentation, Including Capabilities and Procedures,
of the Spin Tunnel Rotary Balance Data Acquisition Program, Bihrle 92-7,
December 1992.
Ralston, John and Avent, John: Rotary Balance Test of a 1/9 Scale General
Dynamics F-16 Model Incorporating Several Mechanical and Pneumatic Vortex
Control Techniques, Bihrle 92-6, October 1992.
Dickes, Edward; Hultberg, Randy; and Ralston, John: Report of Rotary
Balance Wind Tunnel Testing on Generic Forebody Configurations Consisting
of Pressure Measurements and Force and Moment Data Conducted at the
Defense Research Agency Bedford/Farnborugh Facilities, Bihrle 92-5, September
1992.
Bihrle, William Jr., Barnhart, Billy and Avent, John: Analysis of Static
and Rotational Aerodynamics From 0ê through 90ê Angles of Attack for
Rockwell/MBB Fan Ranger, Bihrle 92-2, May 1992.
Ralston, John and Avent, John: Evaluation and Modification of F/A-18B
Aerodynamic Data Base for Improved Departure Modeling, Bihrle 92-2, March
1992.
O'Connor, Cornelius: EA-6B Unified Data Base for Calculation of Aircraft
Motions Between + 90ê Angle of Attack, Bihrle 92-1, March 1992.
Dickes, E., Barnhart, B. and Bihrle,W.Jr.: Analysis of Static and Rotational
Aerodynamics at High Angles of Attack for Rockwell X-31A (F-18 Canopy,
1989 Configuration) Appendix, Exploratory High Alpha Improvement Study,
Bihrle 91-7, October 1991.
Avent, John and Hultberg, Randy: Rotary Balance Tests of a 1/10-Scale
F-16/Vista Model, Bihrle 91-6, September 1991.
O'Connor, Cornelius and Ralston, John: An Update to the High Angle-of-Attack
Data Base of the F-16 OFT Simulation , Bihrle 91-5, September 1991.
Dickes, Edward: An Aerodynamic Math Model of the T-45A Configuration
for Simulation of Flight Motions from -90° to +180° Angle of Attack,
Bihrle 91-4, August 1991.
Dickes, Edward: Rotary Balance Data and Analysis of the T-45A Update
Airplane from -90° to +180° Angle of Attack, Bihrle 91-3, July
1991.
Ralston, John and Barnhart, Billy: Application of Rotary Balance Data
& The Analysis of High of Angle of Attack Characteristics, Bihrle 91-1,
February 1991.
O'Connor, Cornelius: NATC F-18A/B Aerodynamic Math Model Modifications
Incorporated During Phase II Model Unification Report, Bihrle 90-13, September
1990.
Ralston, John: A Low-Speed Aerodynamic Math Model of the Agile Falcon
Airplane from 0° through 90° Angles of Attack, Bihrle 90-12,
June 1990.
Miller, Christopher: AV-8B 100% LERX Rotary Balance Test & Analysis,
Bihrle 90-11, June 1990.
Dickes, Edward: X-31A Low-Speed Aerodynamic Math Model for Simulation
of Aircraft Motions Between -90° and 0° Angles of Attack,
Bihrle 90-9, June 1990.
Mason, Alvin A., Jordan, Samuel W. Jr., Hultberg, Randy S.: Test Report
of Pressure Measurement on the F-16 Airplane During Steady-State Rotational
Motion, Bihrle 90-7, April 1990.
O'Connor, Cornelius: A Low-Speed Aerodynamic Math Model of the YA-7F
Airplane from 0° through 90° Angle of Attack, Bihrle 90-6,
March 1990.
Dickes, Edward: Rotary Balance Tests of an X-31A Model Between -5°
and -90° Angles of Attack, Bihrle 90-3, February 1990.
O'Connor, Cornelius: Rotary Balance Data and Analysis for the Air Force
YA-7F Airplane, Bihrle 90-2, February 1990.
Hultberg, Randy S., Bowman, James S. Jr. and Martin, Colin A.: Measurements
of Pressures on the Tail and Aft Fuselage of An Airplane Model During
Rotary Motions at Spin Attitudes, NASA TP 2939, November 1989.
Miller, Christopher: Rotary Balance Test of Various Electro-Optical
Sensors Mounted on a l/9-scale F-16 MCID Model, Bihrle 89-14, October 1989.
O'Connor, Cornelius and Barnhart, Billy: EA-6B Unified Data Base for
Calculation of Aircraft Motions Between ±90° Angles of
Attack - Phase I Cruise Configuration, Bihrle 89-13, August 1989.
Ralston, John: Analysis of High Angle of Attack Data and Simulation
Results for the F-16 MCID Configuration, Including the Effects of Selected
Stores, Bihrle 89-12, September 1989.
Mason, Alvin: Simulation Results for the Basic Peace Marble II and
the Peace Marble II with a 300-Gallon Centerline Tank, Bihrle 89-10, September
1989.
Dickes, Edward: Incremental Rotational Aerodynamic Math Model of the
Rockwell/MBB X-31A Configuration for Simulation of Flight Motions Between
0° and 90° Angle of Attack, Bihrle 89-9, August 1989.
Dickes, Edward: An Incremental Rotational Aerodynamic Math Model of
the YF-22A Configuration for Simulation of Flight Motions From 0ê Through
90ê Angle of Attack, Bihrle 89-8, May 1989.
Mason, Alvin A.: A Low-Speed Aerodynamic Math Model of the Two-Place
Peace Marble II Configuration With and Without 300-Gallon Centerline
Tank From 0ê through 90ê Angle of Attack, Bihrle 89-7, May 1989.
Mason, Alvin A.: F-16 Peace Marble II Rotary Balance Test Report, Bihrle
89-6, May 1989.
O'Connor, Cornelius: NATC F-18A/B Aerodynamic Math Model Modifications
Incorporated During the Phase I Model Unification Effort, Bihrle 89-5,
March 1989.
Ralston, John: A Low-Speed Aerodynamic Math Model Incorporating the
Effects of the MCID Inlet and Various Stores on the F-16A Airplane from
0° through 90° Angle of Attack, Bihrle 89-4, February 1989.
Bihrle, W. Jr., Barnhart, B., Dickes E.: Influence of Forebody Geometry
on Aerodynamic Characteristics and a Design Guide for Defining Departure/Spin
Resistant Forebody Configurations, Bihrle 89-3, WRDC TR-89-3079, September
1989.
Bihrle, W. Jr., Barnhart, B., Dickes, E.: Static and Rotational Aerodynamic
Data from 0° to 90° Angle of Attack for a Series of Basic
and Altered Forebody Shapes, Bihrle 89-2, WRDC TR-89-3090, February 1989.
Barnhart, B., Ralston, J., O'Connor C.: F-16 NSI Inlet Configuration
Study Including Data, I. Analysis, II. Aerodynamic Math Model, III.
Simulation, Bihrle 89-1, January 1989.
Mason, Alvin: F-16 MCID Inlet Configuration Rotary Balance Test Report,
Bihrle 88-9, December 1988.
Krenkel, Ralph: A Low-Speed Aerodynamic Model of the EA-6B VIP Airplane
in the 0ê to 90ê Angle-of-Attack Range, Bihrle 88-8, November 1988.
Ralston, John N.: Analysis of F-18A/B Low-Speed, High Angle-of-Attack
Aerodynamic Data Base, Including: I. Selected Erect Characteristics,
II. Two-Place Canopy Effect, III. Store Loading Effect, Bihrle 88-7, September
1988.
Mason, Alvin A. and Ralston, John N.: Agile Falcon Rotary Balance Test
Results, Bihrle 88-6, August 1988.
Ralston, John and O'Connor, Cornelius: F-18A/B Low-Speed Aerodynamic
Math Model for Simulation of Aircraft Motions Between -90° and
+90° Angles of Attack, Including: I. Rotational Terms, II. Inverted
Static & Oscillatory Terms, III. Incremental Store Loading Effects,
IV. Two-Place F-18B Canopy Effect, Bihrle 88-5, May 1988.
Ralston, John: A Low-Speed Incremental Aerodynamic Math Model Representing
the Influence of the F-18 Strake Fence, Bihrle 88-4, February 1988.
Ralston, John: Low-Speed Test Data and Analysis of the F-18 Strake
Fence Configuration, Bihrle 88-3, February 1988.
O'Connor, Cornelius, Ralston, John and Barnhart, Billy: An Incremental
Rotational Aerodynamic Math Model of the X-29 Airplane from 0°
Through 90° Angle of Attack, Bihrle 88-2, January 1988.
Dickes, Edward: Analysis of Static and Rotational Aerodynamics at High
Angles of Attack for Rockwell X-31A Preliminary Configuration, Bihrle 88-1,
January 1988.
O'Connor, Cornelius and Ralston, John: A Low-Speed Aerodynamic Math
Model of the F-16A Airplane From 0° Through 90° Angle of
Attack, Bihrle 87-10, November 1987.
Ralston, John N.: An Incremental Rotational Aerodynamic Model of the
SE-5A Configuration for Simulation of Flight Motions in the -90°
to +90° Angle-of-Attack Range, Bihrle 87-9 August 1987.
Hultberg, Randy S. and O'Connor, Cornelius J.: Rotary Balance Data
and Analysis for the Cessna T-48, Bihrle 87-7, June 1987.
Dickes, Edward: Analysis of Static and Rotational Aerodynamics at High
Angles of Attack for the X-EFM/7 Configurations, Bihrle 87-6, May 1987.
Ralston, John: Rotary Balance Data and Analysis for the SE-5A Configuration;
I.- Analysis of Static and Rotational Data at High Angles of Attack,
Bihrle 87-3, April 1987.
Hultberg, Randy: Australian MK-1 Basic Pilot Training Aircraft Pressure
Test Report, Bihrle 87-2, March 1987.
Krenkel, A.R.: Application of Computational Procedures to the Prediction
of High Angle-of-Attack Forebody Aerodynamics. Bihrle 87-1, February 1987.
Bihrle, William Jr., Barnhart, Billy and Dickes, Edward: Analysis of
Static and Rotational Aerodynamics at High Angles of Attack for MBB
SNAKE Configuration, Bihrle 86-11, September 1986.
Dickes, Edward and Barnhart, Billy: An Aerodynamic Math Model of the
MBB SNAKE Airplane for Simulation of Flight Motions in the 0ê to +90ê
Angle-of-Attack Range. Bihrle 86-10, September 1986.
Ralston, John N.: Incremental Aerodynamic Math Model for a Clean EA-6B
Airplane. Bihrle 86-9, June 1986.
Ralston, John N.: A Low-Speed Aerodynamic Model of the Inverted EA-6B
Airplane Through -90° Angle of Attack. Bihrle 86-8, June 1986.
Bihrle, William Jr. and Barnhart, Billy: Analysis of F-14A Static and
Rotational Aerodynamics with Recommended High Angle-of-Attack Flight
Enhancements. Bihrle 86-7, May 1986.
Hultberg, Randy S. and Dickes, Edward G.: A Rotational Aerodynamic
Model of the A-6 Airplane from 0° Through 90° Angle of Attack.
Bihrle 86-6, May 1986.
Hultberg, Randy S. and Dickes, Edward G.: Rotary Balance Data and Analysis
for the Navy A-6A, A-6E and Proposed A-6F Airplanes. Bihrle 86-5, September
1986.
Barnhart, Billy: Incremental Rotational Aerodynamic Math Model for
the F-14D Airplane. Bihrle 86-4, March 1986.
Ralston, John: Incremental Rotational Aerodynamic Math Model of the
X-29 Airplane. Bihrle 86-3, February 1986.
Barnhart, B.: Review of the Static Aerodynamic and Dynamic Derivative
Data Utilized in the F-14A Simulator Math Model. Bihrle 86-2, February
1986.
O'Connor, Cornelius and Barnhart, Billy: Rotary Balance Data and Analysis
for the Navy/Grumman F-14D. Bihrle 86-1, January 1986.
Bihrle, William Jr., Barnhart, Billy, and Dickes, Edward: A Preliminary
Design Guide for Departure/Spin Resistant Forebody Configurations. Bihrle
85-10, January 1986.
Ralston, John: An Aerodynamic Model of the T-46A Trainer for Simulation
of Flight Motions in the -90° to +90° Angle-of-Attack Range.
Bihrle 85-9, November 1985.
Hultberg, Randy: Response of JVX Aircraft to Aggravated Control Inputs.
Bihrle 85-8, July 1985.
Dickes, Edward: Low-Speed Static Aerodynamic Model of the AV-8B Airplane
for an Angle-of-Attack Range of 0° to 90°. Bihrle 85-5, April
1985.
Hultberg, Randy S.: Rotary Balance Data and Analysis for the Bell-Boeing
JVX Airplane, Bihrle 85-1, March 1985.
Dickes, Edward G. and Barnhart, Billy P.: A Low-Speed Aerodynamic Model
of the AV-8B Airplane Through 90° Angle of Attack. Bihrle 85-4, February
1985.
Ralston, John N.: A Low-Speed Aerodynamic Model of the EA-6B Airplane
Through 90ê Angle of Attack. Bihrle 85-3, January 1985.
Dickes, Edward G.: Low Speed T-45 Aerodynamic Model for an Angle-of-Attack
Range of 0° to 90°, Bihrle 85-2, January 1985.
Ralston, John N.: Rotary Balance Data and Analysis for the Navy EA-6B
and Proposed ADVCAP EA-6B Airplanes. I.- Analysis of the High Angle-of-Attack
Aerodynamics and Spins, Bihrle 84-7, November 1984.
Dickes, Edward G.: An Analysis of the High Angle-of-Attack Aerodynamics
and Spins for the Navy T-45 A/B Trainer, Bihrle 84-6, August l984.
Hultberg, Randy S. and Dickes, Edward G.: An Analysis of the High Angle-of-Attack
Aerodynamics and Spins for the Navy AV-8B/TAV-8B Airplanes, Bihrle 84-5,
July 1984.
Ralston, John N. and Jordan, Samuel W. Jr.: Rotary Balance Data and
Analysis for the SAAB JAS-39 Airplane for an Angle-of-Attack Range of
-90° to 90°, Supplementary Study, Bihrle 84-4, June 1984.
Barnhart, Billy: Incremental Rotational Aerodynamic Model for the F-14
Airplane with a 2x4 Store Configuration, Bihrle 84-3, May 1984.
Hultberg, Randy S.: Rotary Balance Model Test Results of the Australian
Aircraft Consortium MK-1 Trainer with Modified Tail Geometries, Bihrle
84-1, January 1984.
Ralston, John and Jordan, Samuel Jr.: Rotary Balance Data and Analysis
for the SAAB JAS-39 Airplane for an Angle-of-Attack Range of -90°
to 90°. Bihrle 83-9, December 1983.
Hultberg, Randy S.: Rotary Balance Data and Analysis for the Australian
Aircraft Consortium MK-1 Trainer. Bihrle 83-7, August 1983.
Barnhart, Billy: F-14 Rotary Balance Tests for an Angle-of-Attack Range
of 0ê to 90ê. NADC-81293-60, Bihrle 82-8, July 1983.
Barnhart, Billy: Incremental Rotational Aerodynamic Model for the F-14
Airplane. Bihrle 83-6, June l983.
Hultberg, Randy S.: Rotary Balance Data for an Angle-of-Attack Range
of 0° to 90° and Predicted Spin Modes for the Westwind Model
1125. Bihrle 83-5, April 1983.
Ralston, John: Rotary Balance Data and Analysis for the Air Force T-46A
Trainer. Bihrle 83-4, April 1983.
Ralston, John: Influence of Fuselage Components, Forebody Shape, and
Wing Planform on the High Angle-of-Attack Rotational Aerodynamics of
the Northrop Design 350. Bihrle 82-10, December 1982.
Hultberg, Randy: Rotary Balance Data for the Rockwell Nova NGT Design
for an Angle-of-Attack Range of 0° to 90°. Bihrle 82-6, June
1982.
Ralston, John: X-29A Rotary Balance Data for an Angle-of-Attack Range
of 0° to 90°. Bihrle 82-5, May 1982.
Ralston, John: Rotary Balance Data for the Fairchild Republic/Air Force
Next Generation Trainer at an Angle-of-Attack Range of -90° to 90°.
Bihrle 81-5, October 1981.
Hultberg, Randy: Rotary Balance Data for the Northrop F-5G and F-5E
Airplanes for an Angle-of-Attack Range of 8° to 90°. Bihrle 81-7, August
1981.
Ralston, John: Spin-Tunnel Investigation of a 1/20-Scale Model of the
Northrop Navy Trainer Configuration 351. Bihrle 81-4, August 1981.
Chu, Julio and Hultberg, Randy: Rotary Balance Data for the Northrop
F-5E Airplane for an Angle-of-Attack Range of 8° to 90°. Bihrle 81-6, June
1981.
Hultberg, Randy: Spin-Tunnel Investigation of a 1/20-Scale Model of
the Northrop Navy Trainer Configuration 350. Bihrle 81-2, March 1981.
Ralston, John: Rotary Balance Data for an Angle-of-Attack Range of
8° to 90° and Estimated Spin Modes for the F-16XL Configuration. Bihrle
81-1, February 1981.
Chu, J., Barnhart, B. and Pantason, P.: Rotary Balance Data for the
Northrop Navy Trainer Configuration 350 for an Angle-of-Attack Range
of 8° to 90°. Bihrle 80-2, October 1980.
Chu, Julio and Hultberg, Randy: Rotary Balance Data for the General
Dynamics Navy Trainer Configuration 603E for an Angle-of-Attack Range
of 8° to 90°. Bihrle 80-1, August 1980.
Bihrle, William Jr., and Barnhart, B.: Influence of Pitching Moment
Characteristics on Departure and Uncoordinated Roll Reversal Boundaries
for Fighter Configurations. AFFDL-TR-79-3157, Bihrle 79-2, February 1980.
Pantason, Paul and Leary, Kevin: Rotary Balance Data for the F-15 and
a Three-Surface Configuration for an Angle-of-Attack Range of 20° to
90°. Bihrle 79-3, July 1979.
Bihrle, William Jr., and Barnhart, B.: Design Charts and Boundaries
for Identifying Departure Resistant Fighter Configurations, NADC-76154-30.
Bihrle 78-3, July 1978.
Ralston, John N.: Rotary Balance Data and Analysis for the X-29A Airplane
for an Angle-of-Attack Range of 0ê to 90ê. NASA CR-3747, Bihrle 83-2, August
1984.
Hultberg, Randy: Low-Speed Rotary Aerodynamics of F-18 Configuration
for 0° to 90° Angle of Attack - Test Results and Analysis. NASA CR-3608,
Bihrle 82-4, August 1984.
Ralston, John N. and Barnhart, Billy P.: Rotary Balance Data for a
Typical Single-Engine General Aviation Design for an Angle-of-Attack
Range of 8° to 90°, III.- Influence of Control Deflection on Predicted
Model D Spin Modes. NASA CR-3248, Bihrle 83-1, June 1984.
Ralston, John: Rotary Balance Data for a Typical Single-Engine General
Aviation Design for an Angle-of-Attack Range of 8° to 90°, I.- Influence
of Airplane Components for Model D. NASA CR-3246, Bihrle 82-7, March 1983.
Barnhart, Billy: Rotary Balance Data for a Typical Single-Engine General
Aviation Design for an Angle-of-Attack Range of 8° to 90°, II.- Influence
of Horizontal Tail Location for Model D. NASA CR-3247, Bihrle 82-2, November
1982.
Barnhart, Billy: Rotary Balance Data for an F-15 Model with Conformal
Fuel Tanks for an Angle-of-Attack Range of 8° to 90°. NASA CR-35l6,
Bihrle 82-3, May 1982.
Barnhart, Billy: F-15 Rotary Balance Data for an Angle-of-Attack Range
of 8° to 90°. NASA CR-3478, Bihrle 81-3, May 1982.
Barnhart, Billy: Analysis of Rotary Balance Data for the F-15 Airplane
Including the Effect of Conformal Fuel Tanks. NASA CR-3479, Bihrle 82-1,
April 1982.
Mulcay, William and Chu, Julio: Rotary Balance Data for a Single-Engine
Agricultural Airplane Configuration for an Angle-of-Attack Range of
8° to 90°. NASA CR-3311, Bihrle 80-6, December 1980.
Mulcay, William and Rose, Robert: Rotary Balance Data for a Typical
Single-Engine General Aviation Design Having a High Aspect-Ratio Canard
for an Angle-of-Attack Range of 30° to 90°. NASA CR-3170, Bihrle 80-3,
December 1980.
Hultberg, Randy, Chu, Julio, and Dickens, Waldo: Rotary Balance Data
for a Typical Single-Engine General Aviation Design for an Angle-of-Attack
Range of 8° to 90°, II.- High Wing Model C. NASA CR-3201, Bihrle 80-5,
October 1980.
Mulcay, William and Rose, Robert: Rotary Balance Data for a Typical
Single-Engine General Aviation Design for an Angle-of-Attack Range of
8° to 90°, I.- Low-Wing Model C. NASA CR-3200, Bihrle 80-4, October 1980.
Hultberg, Randy S. and Mulcay, William: Rotary Balance Data for a Typical
Single-Engine General Aviation Design for an Angle-of-Attack Range of
8° to 90°, I.- Low-Wing Model A. NASA CR-3100, Bihrle 79-7, February 1980.
Bihrle, William Jr. and Mulcay, William: Rotary Balance Data for a
Typical Single-Engine General Aviation Design for an Angle-of-Attack
Range of 8° to 35°, III.- Effect of Wing Leading-Edge Modifications
Model A. NASA CR-3102, Bihrle 79-9, November 1979.
Mulcay, William and Rose, Robert: Rotary Balance Data for a Typical
Single-Engine General Aviation Design for an Angle-of-Attack Range of
8° to 90°, II.- High-Wing Model A. NASA CR-3101, Bihrle 79-8, September
1979.
Bihrle, William Jr. and Hultberg, Randy: Rotary Balance Data for a
Typical Single-Engine General Aviation Design for an Angle-of-Attack
Range of 8° to 90°, II.- Low-Wing Model B. NASA CR-3098, Bihrle 79-5, September
1979.
Bihrle, William Jr. and Hultberg, Randy S.: Rotary Balance Data for
a Typical Single-Engine General Aviation Design for an Angle-of-Attack
Range of 8° to 90°, I.- High-Wing Model B. NASA CR-3097, Bihrle 79-4, September
1979.
Pantason, Paul and Dickens, Waldo: Rotary Balance Data for a Single-Engine
Trainer Design for an Angle-of-Attack Range of 8° to 90°. NASA CR-3099,
Bihrle 79-6, August 1979.
Bihrle, William Jr., Hultberg, Randy S., and Mulcay, William: Rotary
Balance Data for a Typical Single-Engine Low-Wing General Aviation Design
for an Angle-of-Attack Range of 30° to 90°. NASA CR-2972, Bihrle 78-2,
July 1978.
Bihrle, William Jr., Barnhart, Billy, and Pantason, Paul: Static Aerodynamic
Characteristics of a Typical Single-Engine Low-Wing General Aviation
Design for an Angle-of-Attack Range of -8° to 90°. NASA
CR-2971, Bihrle 78-1, July 1978.
Industry Technical Memos
Rotary Balance Tests of F-16 Aft Fuselage Modifications, Bihrle 90-2M, May 1990.
AV-8B 100% LERX Rotary Balance Tests, Bihrle 90-1M, April 10, 1990.
EA-6B MIP High-a Data Review, Bihrle 88-2M, June 8, 1988.
Observations Relative to JAS-39B Rotary Balance Results, Bihrle 88-1M, June 1988.
Documented Demonstration and Validation of I.D.F. SE-5A Configuration High Angle-of-Attack Math Model, Bihrle 87-2M, October 1987.
T-46 Memo, Bihrle 86-6M, October 1986.
Application of Computational Procedures to the Prediction of High Angle-of-Attack Forebody Aerodynamics - Interim Report No. 1. Bihrle
86-5M, July 1986.
A-6 Rotary Balance Data Tapes, Bihrle 86-4M, July 1986.
Status of GAC EA-6B Simulator Math Model, Bihrle 86-3M, April 1986.
Influence of the Presence of LERX on the Rotational Aerodynamic and Spin Characteristics of the T-45A. Bihrle 86-lM, February 1986.
July 1985 Spin Tunnel Velocity Survey, Bihrle 85-lM.
F-14 Dynamic Derivatives, Bihrle 84-9M, December 1984.
Rotary Balance Testing of the AAC Model A-20 (Tandem Seating) Trainer, Bihrle 84-8M, November 1984.
Influence of Cargo Pod and Mods on the High Angle-of-Attack Characteristics of the Cessna 208 Airplane, Bihrle 84-6M, September 1984.
Westwind 1125 Data Tape Information, Bihrle 84-5M, September 1984.
Predicted Dynamic Derivatives for the SAAB JAS-39 as a Function of Rotation Rate From 0° to 90° Angle of Attack, Bihrle 84-4M,
May 1984.
Additional Test Requirements for a T-46 Simulator Aero Model, Bihrle 84-3M, April 1984.
JAS-39 Rotary Balance Data Tapes, Bihrle 84-2M, January 1984.
Exploratory Investigation of an Additional Longitudinal Control Device, Wing Mods, and Forebody Strake on the JAS-39 Airplane, Bihrle
84-1M, January 1984.
Effect of Reynolds Number on the High Angle-of-Attack Pitching Moment Characteristics of Military Airplanes, Bihrle 83-2M, September
1983.
Velocity and Rotation Rate Requirements for Rotary Balance Testing, Bihrle 83-lM, July 1983.
Analysis of Rotary Balance Data for the Rockwell Nova NGT Design, Bihrle 82-1M, August 1982.
Determination of Parachute Size and Riser Length Needed for Satisfactory Spin Recovery on the Northrop Navy Trainer Configuration 350,
Bihrle 81-11M, November 1981.
Effect of Lateral Weight Asymmetry on Predicted F-5E Inverted Spin Modes, Bihrle 81-10M, August 1981.
Effect of Pitching Moment Variations on the Predicted Spin Modes of General Aviation Airplanes, Bihrle 81-9M, June 1981.
Status of Dynamic Derivative Prediction for a Spinning Airplane, Bihrle 81-8M, August 1988.
A Review of Leading-Edge Modifications on Rotary Aerodynamic Data for General Aviation Aircraft, Bihrle 81-7M, May 1981.
Effect of Lateral Mass Asymmetries on the Spin Modes of the General Aviation Airplane Model A with Horizontal Tail Configuration 3,
Bihrle 81-6M, May 1981.
Predicted Spin Modes for General Aviation Airplanes, Bihrle 81-5M, April 1981.
Spin Tunnel Flow Survey to Identify Accuracy of Angle of Attack and Sideslip Angle Settings, Bihrle 81-4M, March 1981.
The Influence of Altitude and Inertia Values on Spin Characteristics, Bihrle 81-3M, February 1981.
Influence of Strakes, Wing Tips on VTX Configuration, Bihrle 81-2M, February 1981.
The Influence of Inertia Parameter Variations on the Spin Characteristics of a Typical Low-Wing General Aviation Airplane, Bihrle 81-1M,
February 1981.
Rotary Balance Data for the Grumman/Beech Design 730 VTX Airplane, Bihrle 80-5M, September 1980.
Rotational Aerodynamics for the Fairchild/Republic Generalized NGT Configuration Study, Bihrle 80-4, May 1980.
Rotary Balance Data for the Piper Design #41 Airplane, Bihrle 80-3M, January l980.
Program Performance Spec. for Flight Controls Module, Bihrle 80-2M, December l979.
Program Performance Spec. for F-18 Dynamics Module for Part Task Simulator, Bihrle 80-1M, December 1979.
Analytical Spin Time Histories for a Typical Low-Wing Single-Engine General Aviation Airplane, Bihrle 79-3M, June 1979.
February 1979 Spin Tunnel Velocity Survey, Bihrle 79-2M.
Estimated Dynamic Aerodynamic Derivatives for the LWGA (Yankee) for the -8û to 90û Angle-of-Attack Range, Bihrle 79-lM,
January 1979.
Aerodynamic Model for the T-34C Flight Instrument Trainer, Bihrle 78-12M, October 1978.
YT-34C Airplane - Aerodynamic Natural Frequencies, Damping Ratios, and Static Gains - Longitudinal and Lateral/Directional Modes, Bihrle
78-10M, November 1978.
LWGA Spin Equilibrium Conditions - Comparison of Analytical Estimates from Rotary Balance Wind Tunnel Test Observations.
Configurations: BWLH3V and BWLH4V, Bihrle 78-9M, July 3, 1978.
Static Force Testing of the T-34C l/6 and l/15-Scale Models in the 12-Foot Tunnel, Bihrle 78-8M, May l978.
Demonstration of New Data Acquisition System in Langley 12-Foot Tunnel, Bihrle 78-7M, February 1978.
Evaluation and Comments on the Aerodynamic Tolerances Specified for the T-34C Aircraft Flight Instrument Trainer, Bihrle 78-6M, May
1978.
Evaluation and Comments on the Beech Aerodynamic Data Submittal for the T-34C Flight Instrument Trainer, Bihrle 78-5M, May 1978.
Six Degree-of-Freedom Program Available for Spin Studies, Bihrle 78-4M, March 1978.
Rotary Balance Data Acquisition, Reduction, and Plotting Equipment, Bihrle 78-3M, February, 1978.
Testing of 1/7-Scale Yankee Model on Ames Rotary Balance Apparatus, Bihrle 78-2M, April 1978.
Radio Control Model Data Reduction - General Aviation Program, Bihrle
78-1M, February 1978.
