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 abstract in SAE -- J v 69 n 7 July 1961 p 32-6)
Supersonic transport -- Required characteristics of configurations
SAE -- Paper
SAE Meeting ; 1961 Supersonic
1961
12 pages
Conference paper
English
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