Parametric studies on ground vibration test modeling for highly flexible aircraft

Journal of Aircraft

Volumn 44, Issue 6, 2007, Pages 2049-2059

  Chang, Chong Seok ^a,b,c   Hodges, Dewey H ^a,b,c  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b School of Aerospace Engineering

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; FINITE ELEMENT METHOD; NONLINEAR ANALYSIS; PARAMETER ESTIMATION; VIBRATIONS (MECHANICAL); WINGS;

FLYING WINGS; GEOMETRIC CONSTRAINTS; HIGHLY FLEXIBLE AIRCRAFT;

GROUND EFFECT;

EID: 38149035195     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.30733     Document Type: Article

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