Influence of external store aerodynamics on flutter/LCO of a fighter aircraft

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2002, Pages 1625-1635

  Chen, P C ^a   Sulaeman, E ^a   Liu, D D ^a   Denegri Jr , C M ^a  

^a ZONA TECHNOLOGY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; CORRELATION METHODS; DAMPING; FIGHTER AIRCRAFT; MATHEMATICAL MODELS; MATRIX ALGEBRA; OSCILLATIONS; STABILITY CRITERIA; STRUCTURAL ANALYSIS;

EXTERNAL STORE AERODYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 0036072719     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1410     Document Type: Conference Paper

References (17)

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3. Transonic AIC approach for aeroelastic and MDO applications
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5. Piston theory revisited and further applications
6. Interpolation using surface splines
7. Splines minimizing rotation-invariant semi-norms in sobolev spaces
8. A damping perturbation method for flutter solution: The g-method
9. YF-16 active control system/structural dynamics interaction instability
10. Limit cycle oscillation characteristics of fighter aircraft
11. An application of the P-transform method for transient maneuvering analysis
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13. Adaptive reconfigurable control based on a reduced order system identification for flutter and aeroservoelastic instability suppression
14. Limit cycle oscillation flight test results of a fighter with external stores