F-16 limit cycle oscillation testing with asymmetric stores

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 328-334

  Dawson, Kenneth S ^a   Sussingham, J Chris ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; FLUTTER (AERODYNAMICS); SOFTWARE TESTING;

AERODYNAMIC MODELING; AERODYNAMIC MODELS; ANALYTICAL RESULTS; ASYMMETRIC CONFIGURATIONS; FLIGHT TEST DATA; FLUTTER INSTABILITY; GOOD CORRELATIONS; LIMIT CYCLE OSCILLATION (LCO);

SUPERSONIC AIRCRAFT;

EID: 84964311108     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-3142     Document Type: Conference Paper

References (0)