Problems resulting from increased temperature associated with high speed flight investigated at Lockheed research laboratory; means available for solving such problems for structures flying in intermediate hypersonic range; subject considered under three headings: aerodynamic heating, structural configurations for thermal flight, and production problems. (see also abstracts in Automotive Industries v 116 n 9 May 1 1957 p 126-7; Western Metals v 15 n 8 Aug 1957 p 51-4; Soc Automotive Engrs -- J v 65 n 9 Aug 1957 p 38-42)
Problems in application of high strength steel alloys in design of supersonic aircraft
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957 Steel
1957
42 pages
Conference paper
English
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Problems in application of high strength steel alloys in design of supersonic aircraft
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