Review of changes in aircraft design in recent years; problems associated with flight at extremely high speed, development of integral construction, and aircraft designed to fly in high subsonic and supersonic regimes; steel honeycomb sandwich construction and core development; design features of Cranfield project A-60 supersonic airliners to fly at 1450 mph at altitudes between 57,000-65,000 ft, including structure, power plant, pressurization and air conditioners, and fuel system. (See also Production Engr v 41 n 7 July 1962 p 394-415)
Design trends -- Aircraft
Aircraft Eng
Aircraft Engineering ; 34 , n 399
1962
8 pages
Article (Journal)
English
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