Random aeroelastic response due to strong hypersonic unsteady-wave/shock interaction with acoustic loads

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

Volumn 4, Issue , 2007, Pages 3869-3878

  Kim, Kwangkeun ^a,c   Kim, Young Chan ^a,c   Mignolet, Marc P ^a,c,d   Liu, Danny D ^a,c,d   Chen, Ping Chih ^b,d   Lee, Dong Hwan ^b,d  

^a ARIZONA STATE UNIVERSITY   (United States)

^b ZONA TECHNOLOGY INC   (United States)

^c Department of Mechanical and Aerospace Engineering ^*  (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTICS; HYPERSONIC AERODYNAMICS; MATHEMATICAL MODELS; SHOCK WAVES; SUPERSONIC AIRCRAFT;

ACOUSTIC EXCITATION; ACOUSTIC LOADS; HYPERSONIC AIR VEHICLE PANELS; STRUCTURAL RESPONSES;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 34547507600     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-2014     Document Type: Conference Paper

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