Response of Launch Pad Structures to Random Acoustic Excitation

The design of launch pad structures, particularly those having a large area-to-mass ratio, is governed by launch-induced acoustics, a relatively short transient with random pressure amplitudes having a non-Gaussian distribution. The factors influencing the acoustic excitation and resulting structura...

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Main Authors: Ravi N. Margasahayam, Raoul E. Caimi
Format: Article
Language:English
Published: Wiley 1994-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.3233/SAV-1994-1407
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author Ravi N. Margasahayam
Raoul E. Caimi
author_facet Ravi N. Margasahayam
Raoul E. Caimi
author_sort Ravi N. Margasahayam
collection DOAJ
description The design of launch pad structures, particularly those having a large area-to-mass ratio, is governed by launch-induced acoustics, a relatively short transient with random pressure amplitudes having a non-Gaussian distribution. The factors influencing the acoustic excitation and resulting structural responses are numerous and cannot be predicted precisely. Two solutions (probabilistic and deterministic) for the random vibration problem are presented in this article from the standpoint of their applicability to predict the response of ground structures exposed to rocket noise. Deficiencies of the probabilistic method, especially to predict response in the low-frequency range of launch transients (below 20 Hz), prompted the development of the deterministic analysis. The relationship between the two solutions is clarified for future implementation in a finite element method (FEM) code.
format Article
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institution Kabale University
issn 1070-9622
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language English
publishDate 1994-01-01
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record_format Article
series Shock and Vibration
spelling doaj-art-38c88433381240faa6e8d867fda6fe2d2025-08-20T03:55:11ZengWileyShock and Vibration1070-96221875-92031994-01-011437538410.3233/SAV-1994-1407Response of Launch Pad Structures to Random Acoustic ExcitationRavi N. Margasahayam0Raoul E. Caimi1I-NET Space Services, I-NET Inc., Mail Stop INI-5, John F. Kennedy Space Center, FL 32899, USANASA Engineering Development, Mail Stop DM-MED-11, John F. Kennedy Space Center, FL 32899, USAThe design of launch pad structures, particularly those having a large area-to-mass ratio, is governed by launch-induced acoustics, a relatively short transient with random pressure amplitudes having a non-Gaussian distribution. The factors influencing the acoustic excitation and resulting structural responses are numerous and cannot be predicted precisely. Two solutions (probabilistic and deterministic) for the random vibration problem are presented in this article from the standpoint of their applicability to predict the response of ground structures exposed to rocket noise. Deficiencies of the probabilistic method, especially to predict response in the low-frequency range of launch transients (below 20 Hz), prompted the development of the deterministic analysis. The relationship between the two solutions is clarified for future implementation in a finite element method (FEM) code.http://dx.doi.org/10.3233/SAV-1994-1407
spellingShingle Ravi N. Margasahayam
Raoul E. Caimi
Response of Launch Pad Structures to Random Acoustic Excitation
Shock and Vibration
title Response of Launch Pad Structures to Random Acoustic Excitation
title_full Response of Launch Pad Structures to Random Acoustic Excitation
title_fullStr Response of Launch Pad Structures to Random Acoustic Excitation
title_full_unstemmed Response of Launch Pad Structures to Random Acoustic Excitation
title_short Response of Launch Pad Structures to Random Acoustic Excitation
title_sort response of launch pad structures to random acoustic excitation
url http://dx.doi.org/10.3233/SAV-1994-1407
work_keys_str_mv AT ravinmargasahayam responseoflaunchpadstructurestorandomacousticexcitation
AT raoulecaimi responseoflaunchpadstructurestorandomacousticexcitation