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; 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
Automotive Industries
Automotive Industries ; 116 , n 9 ; p 126-127
1957
2 pages
Aufsatz (Zeitschrift)
Englisch
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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
|Practical Structural Design Problems of Supersonic Aircraft
Emerald Group Publishing | 1957
|