NASA NTRS · 19790013254
Recent advances in convectively cooled engine and airframe structures for hypersonic flight
Abstract
A 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.
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Kelly, H. N., Wieting, A. R., Shore, C. P., Nowak, R. J.. 1978-01-01. Recent advances in convectively cooled engine and airframe structures for hypersonic flight. https://ntrs.nasa.gov/citations/19790013254
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