Overall configuration requirements which represent view of group conducting research at NASA Langley Research Center; problem areas of takeoff noise, sonic boom, airframe and engine life; examination of cruise performance, stability, materials and structures, aeroelastic considerations, and engine configurations; advances in performance capability and operational flexibility can be achieved through incorporation of variable wing sweep and advanced fan type engine. (See also SAE -- Paper 341F for meeting Apr 4-7 1961 12 p)
Supersonic transport -- Required characteristics of configurations
SAE -- J
Society of Automotive Engineers -- Journal ; 69 , n 7
1961
5 pages
Article (Journal)
English
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