Design minimization of noise in stiffened cylinders due to tonal external excitation

Journal of Aircraft

Volumn 36, Issue 3, 1999, Pages 563-570

  Cunefare, Kenneth A ^a   Crane, Scott P ^a,b   Engelstad, Stephen P ^c   Powell, Eugene A ^c  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b FORD MOTOR COMPANY   (United States)

^c LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC VARIABLES CONTROL; BOUNDARY ELEMENT METHOD; CABINS (AIRCRAFT); COMPUTER SIMULATION; CYLINDERS (SHAPES); FINITE ELEMENT METHOD; FREQUENCY RESPONSE; OPTIMIZATION; WEIGHT CONTROL;

ACOUSTIC RESPONSE; SHELL THICKNESS; STIFFENED CYLINDERS; STRUCTURAL WEIGHT;

AIRCRAFT;

EID: 0033132741     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2471     Document Type: Article

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