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Recent advances in convectively cooled engine and airframe structures for hypersonic flightA hydrogen-cooled structure for a fixed-geometry, airframe-integrated scramjet is described. The thermal/structural problems, concepts, design features, and technological advances are applicable to a broad range of engines. Convectively cooled airframe structural concepts that have evolved from an extensive series of investigations, the technology developments that have led to these concepts, and the benefits that accrue from their use are discussed.
Document ID
19790013254
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelly, H. N. (NASA Langley Research Center Hampton, VA, United States)
Wieting, A. R. (NASA Langley Research Center Hampton, VA, United States)
Shore, C. P. (NASA Langley Research Center Hampton, VA, United States)
Nowak, R. J. (NASA Langley Research Center Hampton, VA, United States)
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
Meeting Information
Meeting: Congr. of the Intern. Council of the Aeron. Sci.
Location: Lisbon
Start Date: September 10, 1978
End Date: September 16, 1978
Accession Number
79N21425
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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