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Thermostructural analysis of a scramjet fuel-injection strutResults of a thermal/structural design analysis study of a fuel injection strut for an airframe integrated hydrogen cooled scramjet are presented. It is indicated that a feasible thermal/structural concept has been identified for the static load conditions and that thermal stresses dominate the response. It is suggested that the response of the concept to dynamic loads be investigated.
Document ID
19790013256
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wieting, A. R. (NASA Langley Research Center Hampton, VA, United States)
Thornton, E. A. (Old Dominion Univ.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: Recent Advan. in Structures for Hypersonic Flight, Pt. 1
Subject Category
Structural Mechanics
Accession Number
79N21427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19790013251Collected WorksRecent Advances in Structures for Hypersonic Flight, Part 1
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