Lower-order aerodynamic loads modeling of a maneuvering generic fighter using DDES simulations

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Jeans, Tiger L ^a   McDaniel, David R ^b   Cummings, Russell M ^a   Bergeron, Keith ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC INSTABILITY; AERODYNAMIC MODELS; AIRCRAFT CONFIGURATIONS; AIRCRAFT SYSTEM IDENTIFICATION; CFD SIMULATIONS; COMPUTATIONAL TOOLS; CONSTANT FREQUENCY; DESIGN PROCESS; DEVELOPMENT COSTS; FLIGHT ENVELOPE; FLIGHT TEST; FREQUENCY CHIRP; HANDLING QUALITY; HIGH FIDELITY; MODELING AND SIMULATION; MODELING TECHNIQUE; NON-LINEAR AERODYNAMICS; NONLINEAR FLOW; REDUCED ORDER MODELS; STABILITY AND CONTROL; STRONGLY NONLINEAR; UNITED STATES AIR FORCE;

AERODYNAMIC LOADS; AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FORECASTING;

AERODYNAMIC CONFIGURATIONS;

EID: 78549295890     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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