Computation of limit cycle oscillations of a delta wing

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

Volumn 3, Issue , 2002, Pages 1636-1646

  Gordnier, Raymond E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; OSCILLATIONS;

DELTA WINGS;

WINGS;

EID: 0036078315     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1411     Document Type: Conference Paper

References (31)

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3. Practical problems: Airplanes
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5. Effects of angle of attack on nonlinear flutter of a delta wing
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8. An implicit factored scheme for the compressible navier-stokes equations
9. A diagonal form of an implicit approximate-factorization algorithm
10. The computed structure of a 3-D turbulent interaction caused by a cylinder/offset flare juncture
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12. Semianalytical solution of rectangular plates