Supersonic aeroelastic instability results for a NASP-like wing model

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

Volumn , Issue pt 1, 1993, Pages 638-647

  Cole, Stanley R ^a   Florance, James R ^a   Thomason, Lee B ^a   Spain, Charles V ^a   Bullock, Ellen P ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AIRFOILS; DYNAMIC LOADS; DYNAMIC RESPONSE; MATHEMATICAL MODELS; MODELS; PRESSURE EFFECTS; STABILITY; SUPERSONIC AERODYNAMICS; WIND TUNNELS;

LANGLEY UNITARY PLAN WIND TUNNEL FACILITY; NATIONAL AEROSPACE PLANE (NASP); STATIC DIVERGENCE;

WINGS;

EID: 0027287030     PISSN: 01615750     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)