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 Soc Automotive Engrs -- Paper n 84 for meeting Apr 2-5 1957 42 p; 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)
Problems in application of high strength steel alloys in design of supersonic aircraft
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 65 , n 9 ; p 38-42
1957
5 pages
Article (Journal)
English
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Problems in application of high strength steel alloys in design of supersonic aircraft
Engineering Index Backfile | 1957
|Problems in application of high strength steel alloys in design of supersonic aircraft
Engineering Index Backfile | 1957
|Problems in the Application of High-Strength Steel Alloys in the Design of SUPERSONIC Aircraft
SAE Technical Papers | 1958
|Unique structural problems in supersonic aircraft design
Engineering Index Backfile | 1956
|