Method of predicting quasi-steady aerodynamics for flutter analysis of high speed vehicles using steady CFD calculations

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

Volumn , Issue pt 1, 1993, Pages 595-603

  Scott, Robert C ^a   Pototzky, Anthony S ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AEROSPACE VEHICLES; APPROXIMATION THEORY; COMPUTATIONAL METHODS; FLUID STRUCTURE INTERACTION; SHOCK WAVES; STRUCTURAL ANALYSIS; UNSTEADY FLOW; VISCOUS FLOW; WINGS;

COMPUTATIONAL FLUID DYNAMICS (CFD); NEWTONIAN IMPACT THEORY; PISTON THEORY; QUASISTEADY AERODYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 0027151050     PISSN: 01615750     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)