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Validation of a Deterministic Vibroacoustic Response Prediction ModelThis report documents the recently completed effort involving validation of a deterministic theory for the random vibration problem of predicting the response of launch pad structures in the low-frequency range (0 to 50 hertz). Use of the Statistical Energy Analysis (SEA) methods is not suitable in this range. Measurements of launch-induced acoustic loads and subsequent structural response were made on a cantilever beam structure placed in close proximity (200 feet) to the launch pad. Innovative ways of characterizing random, nonstationary, non-Gaussian acoustics are used for the development of a structure's excitation model. Extremely good correlation was obtained between analytically computed responses and those measured on the cantilever beam. Additional tests are recommended to bound the problem to account for variations in launch trajectory and inclination.
Document ID
19970016845
Acquisition Source
Kennedy Space Center
Document Type
Technical Memorandum (TM)
Authors
Caimi, Raoul E.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Margasahayam, Ravi
(I-NET, Inc. Cocoa Beach, FL United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-112649
NAS 1.15:112649
Report Number: NASA-TM-112649
Report Number: NAS 1.15:112649
Accession Number
97N19230
Funding Number(s)
CONTRACT_GRANT: NAS10-11943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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