Nonlinear modeling of unsteady aerodynamics at high angle of attack

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2004, Pages 1213-1230

  Allwine, Daniel A ^a,e   Strahler, Jeremy A ^a,e   Lawrence, Douglas A ^b,f   Jenkins, Jerry E ^c,e   Myatt, James H ^d  

^a Austral Engineering and Software Inc   (United States)

^b OHIO UNIVERSITY   (United States)

^c Austral Engineering and Software Inc   (United States)

^d AIR FORCE RESEARCH LABORATORY   (United States)

^e AFRL/VACA ^*

^f School of EECS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; COMPUTER SIMULATION; CONTROL SYSTEMS; MATHEMATICAL MODELS; STATE SPACE METHODS; SYSTEMS ANALYSIS; UNSTEADY FLOW; WINGS;

CONTROL SYSTEM DESIGN; DELTA WING; NONLINEAR INDICIAL RESPONSE (NIR); UNSTEADY AERODYNAMICS;

AERODYNAMICS;

EID: 19644389500     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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3. Grismer, D.S., Myatt, J.H., McKeehan P.D., and Buffington, J.M., "Application of a Nonlinear-Indicial-Response Model to a Tailless Aircraft Simulation," AIAA Paper 97-3644, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug. 1997.
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11. Myatt, J.H., Modeling the Rolling Moment on the 65-Degree Delta Wing for Rolling Motions at High Angle of Attack, Ph.D. Dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, 1997.
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