Transverse vibration analysis for partly wrinkled membranes

Journal of Spacecraft and Rockets

Volumn 43, Issue 3, 2006, Pages 626-637

  Hossain, N M A ^a,d,e   Jenkins, C H ^a,e,f,g   Woo, K ^b,e,h   Igawa, H ^c,i  

^a SOUTH DAKOTA SCHOOL OF MINES AND TECHNOLOGY   (United States)

^b Chungbuk National University   (South Korea)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d Mechanical Engineering Department   (United States)

^e AIAA   (United States)

^f MS 11 B

^g MONTANA STATE UNIVERSITY   (United States)

^h CAE

ⁱ Institute of Space Technology and Aeronautics   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; FINITE ELEMENT METHOD; SPACECRAFT;

MEMBRANE-BASED WRINKLE ALGORITHM; MODE SHAPES; TRANSVERSE VIBRATION BEHAVIOR; WRINKLING AFFECTS;

VIBRATION MEASUREMENT;

EID: 33745737630     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.11327     Document Type: Conference Paper

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