Effects of spoiler surfaces on the aeroelastic behavior of a low-aspect-ratio rectangular wing

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

Volumn , Issue pt 3, 1990, Pages 1455-1463

  Cole, Stanley R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT--WINGS; FLUID DYNAMICS--MATHEMATICAL MODELS; STRUCTURAL ANALYSIS--DYNAMIC RESPONSE; WIND TUNNELS;

LANGLEY TRANSONIC DYNAMICS TUNNEL; RECTANGULAR WING; SPOILER SURFACES;

AERODYNAMICS;

EID: 0025252943     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)