Nonlinear random response of panels in an elevated thermal-acoustic environment

Journal of Aircraft

Volumn 40, Issue 4, 2003, Pages 683-691

  Dhainaut, Jean Michel ^a   Guo, Xinyun ^a   Mei, Chuh ^a   Spottswood, S Michael ^b   Wolfe, Howard F ^b  

^a Old Dominion University   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; AIRCRAFT PARTS AND EQUIPMENT; DEGREES OF FREEDOM (MECHANICS); FINITE ELEMENT METHOD; HIGH TEMPERATURE EFFECTS; INTEGRATION; LAMINATED COMPOSITES; NONLINEAR EQUATIONS; PRESSURE; STIFFNESS MATRIX; STRAIN; THERMAL LOAD;

ACOUSTIC LOADS; ELEVATED THERMAL-ACOUSTIC ENVIRONMENT; LAMINATED COMPOSITE PANEL; NONLINEAR MODAL STIFFNESS MATRIX;

AEROSPACE ENGINEERING;

EID: 0042882641     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3146     Document Type: Article

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