Ground vibration testing master class: Modern testing and analysis concepts applied to an F-16 aircraft

Conference Proceedings of the Society for Experimental Mechanics Series

Volumn 1, Issue , 2011, Pages 221-228

  Lau, Jenny ^a   Peeters, Bart ^a   Debille, Jan ^a   Guzek, Quentin ^a   Flynn, Willam ^a   Lange, Donald S ^b   Kahlmann, Timo ^c  

^a LMS INTERNATIONAL   (Belgium)

^b Air Force Flight Test Center ^*  (United States)

^c AICON 3D Systems GmbH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT STRUCTURE; ANALYSIS RESULTS; ANALYSIS TIME; DEVELOPMENT PROCESS; F-16 AIRCRAFTS; GROUND VIBRATION TESTING; INTEGRATED APPROACH; MODAL TESTINGS; MODEL UPDATING; MULTIPLE CONFIGURATIONS; NUMERICAL MODELS; SAFETY-CRITICAL; TEST RESULTS; TIME PRESSURES; VIBRATION DATA;

AEROSPACE APPLICATIONS; AIRCRAFT MANUFACTURE; AIRCRAFT MODELS; AIRFRAMES; FLUTTER (AERODYNAMICS); MODAL ANALYSIS; PNEUMATIC CONTROL EQUIPMENT; STRUCTURAL ANALYSIS; STRUCTURAL DYNAMICS;

VIBRATION ANALYSIS;

EID: 79958104699     PISSN: 21915644     EISSN: 21915652     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

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3. S. Pauwels, Experimental Modal Analysis: Efficient geometry model creation using optical techniques, In Proc. 75th Shock 1 vibration Symposium, 2004
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5. D. L. Hunt, A comparison of methods for aircraft ground vibration testing, In Proc. IMAC III International Modal Analysis Conference, 1985
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7. D. Göge, Ground Vibration Testing of Large Aircraft - State-of-the-Art and future perspectives, In Proc. IMAC XXV International Modal Analysis Conference, 2007