Experimental unsteady pressures at flutter on the supercritical wing benchmark model

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

Volumn , Issue pt 5, 1993, Pages 2504-2514

  Dansberry, Bryan E ^a   Durham, Michael H ^a   Bennett, Robert M ^a   Rivera, Jose A ^a   Silva, Walter A ^a   Wieseman, Carol D ^a   Turnock, David L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); FLUID DYNAMICS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; PRESSURE MEASUREMENT; TRANSONIC AERODYNAMICS; WIND TUNNELS;

FLUTTER TESTING; LANGLEY TRANSONIC DYNAMICS TUNNEL; PITCH AND PLUNGE APPARATUS (PAPA); SUPERCRITICAL WING (SW) BENCHMARK MODEL;

WINGS;

EID: 0027208455     PISSN: 01615750     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)