Reduced order modeling of X-31 wind tunnel model aerodynamic loads

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Jirásek, Adam ^a,b,c   Cummings, Russell M ^a,c  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b NATIONAL RESEARCH COUNCIL   (United States)

^c Department of Aeronautics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT CONTROL; FLIGHT CONTROL SYSTEMS; NAVIER STOKES EQUATIONS; RELIGIOUS BUILDINGS; RESEARCH AIRCRAFT; TRAINING AIRCRAFT; WIND TUNNELS;

AIRCRAFT CONFIGURATIONS; COMPUTATIONAL TECHNIQUE; LOW-SPEED WIND TUNNEL; NON-LINEAR AERODYNAMICS; PREDICTIVE CAPABILITIES; STABILITY AND CONTROL; STATIC AND DYNAMIC INSTABILITIES; SYSTEM IDENTIFICATION METHODS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78649520216     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4693     Document Type: Conference Paper

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