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A generalized dynamic aerodynamic coefficient model for flight dynamics applications

Published:1997-08-11 Issue: Volume: Page:
ISSN:
Container-title:22nd Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Lin Guo-Feng¹,Lan C.¹,Brandon Jay²,Lin Guo-Feng¹,Lan C.¹,Brandon Jay²

Affiliation:

1. Kansas, Univ., Lawrence

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3643

Reference34 articles.

1. 1Etkin,B.,DynamicsofAtmosphericFlight,Wiley,New York, 1972.

2. Dynamic Stability Parameters, AGARDLS-114, 1981.

3. Grafton, S. B. and Libbey, C. E. "Dynamic Stability Derivatives of aTwin-JetFighterModelfor AnglesofAttack from -10° to 110°,"NASA TND-6091, 1971.

4. 4Tobak,M.andSchiff,L.B."AerodynamicModeling- Basic Concepts",inDynamicStabilityParameters* AGARDLS-114, 1981.

5. Chambers, J. R. and Grafton, S. B. "Aerodynamic CharacteristicsofAirplanes atHigh Angles of Attack,"NASA TM-74097,1977.

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