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High Speed Research Program Sonic FatigueThe objective of this sonic fatigue summary is to provide major findings and technical results of studies, initiated in 1994, to assess sonic fatigue behavior of structure that is being considered for the High Speed Civil Transport (HSCT). High Speed Research (HSR) program objectives in the area of sonic fatigue were to predict inlet, exhaust and boundary layer acoustic loads; measure high cycle fatigue data for materials developed during the HSR program; develop advanced sonic fatigue calculation methods to reduce required conservatism in airframe designs; develop damping techniques for sonic fatigue reduction where weight effective; develop wing and fuselage sonic fatigue design requirements; and perform sonic fatigue analyses on HSCT structural concepts to provide guidance to design teams. All goals were partially achieved, but none were completed due to the premature conclusion of the HSR program. A summary of major program findings and recommendations for continued effort are included in the report.
Document ID
20050160468
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Rizzi, Stephen A.
(NASA Langley Research Center Hampton, VA, United States)
Beier, Theodor H.
(Boeing Co. Saint Louis, MO, United States)
Heaton, Paul
(Boeing Co. Saint Louis, MO, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2005
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/CR-2005-213742
Report Number: NASA/CR-2005-213742
Funding Number(s)
WORK_UNIT: WU 537-06-37-20
CONTRACT_GRANT: NAS1-20220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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