Nonlinear rate and amplitude effects on a generic combat aircraft model

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Ericsson, Lars E ^a   Beyers, Martin E ^b  

^a Institute for Aerospace Research ^*  (United States)

^b NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; DEGREES OF FREEDOM (MECHANICS);

ANGULAR AMPLITUDE; CONCEPTUAL ANALYSIS; DEGREE OF FREEDOM; DYNAMIC EXPERIMENT; LARGE AMPLITUDE; NONLINEAR EFFECT; UNSTEADY AERODYNAMICS; UNSTEADY SEPARATED FLOW;

FIGHTER AIRCRAFT;

EID: 84983156940     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-409     Document Type: Conference Paper

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