On prediction of aircraft trajectory at high-angles of attack: Preliminary results for a pitching airfoil

AIAA Modeling and Simulation Technologies Conference and Exhibit

Volumn , Issue , 2008, Pages

  Bacic, Marko ^a  

^a Department of Engineering Science ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC FORCES; AIRCRAFT TRAJECTORY; ANGLES OF ATTACK; DYNAMIC WIND TUNNELS; FLIGHT ENVELOPE; HARD-WARE-IN-THE-LOOP; HIGH ANGLES OF ATTACK; NONLINEAR MATHEMATICAL MODEL; PITCHING AIRFOILS; RESEARCH EFFORTS; UNMANNED AIRCRAFTS; UNSTEADY AERODYNAMICS;

AIRCRAFT; AIRFOILS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; COMPUTER SIMULATION; FLIGHT ENVELOPES; FORECASTING; FREE FLIGHT; MATHEMATICAL MODELS;

FLIGHT CONTROL SYSTEMS;

EID: 78651067959     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

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