Identification of experimental unsteady aerodynamic impulse responses

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

Volumn 7, Issue , 2003, Pages 5086-5095

  Silva, Walter A ^a   Piatak, David J ^a   Scott, Robert C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FREQUENCIES; IMPULSE RESPONSE; MATHEMATICAL MODELS; OSCILLATIONS; PRESSURE TRANSDUCERS; STEP RESPONSE; UNSTEADY FLOW; WINGS;

RIGID SEMISPAN MODEL; TRANSONIC DYNAMIC TUNNEL; UNSTEADY AERODYNAMIC IMPULSE RESPONSE;

TRANSONIC AERODYNAMICS;

EID: 0041475894     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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11. Corliss, J. M. and Cole, S. R., "Heavy Gas Conversion of the NASA Langley Transonic Dynamics Tunnel," Proceedings of the 20th Advanced Measurements and Ground Testing Technology Conference, No. 98-2710, Albuquerque, NM, June 1998.
12. Cole, S. R. and Rivera Jr, J. A., "The New Heavy Gas Testing Capability in the NASA Langley Transonic Dynamics Tunnel," Royal Aeronautical Society Wind Tunnels and Wind Tunnel Test Techniques Forum, No. 4, Cambridge, UK, April 1997.
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14. Dansberry, B. E., Durham, M. H., Bennett, R. M., Rivera, J. A., Silva, W. A., and Wieseman, C. D., "Experimental Unsteady Pressures at Flutter on the Supercritical Wing Benchmark Model," AIAA/ASME/ASCE/AIIS/ASC 34th Structures, Structural Dynamics, and Materials Conference, La Jolla, CA, April 1993.
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