1976•NASA STI Repository (National Aeronautics and Space Administration)Open access

Aerodynamic Performance Studies for Supersonic Cruise Aircraft

V. R. Mascitti

Abstract

Technical progress made in each of the disciplinary research areas affecting the design of supersonic cruise aircraft is discussed. The NASA Supersonic Cruise Aircraft Research program has supported an expanded research program in aerodynamics including an ever growing experimental data base, methodology development across the Mach number range, and sonic boom. Progress in the aerodynamics area could facilitate the choice of the highly swept subsonic leading edge, arrow wing, known for superior supersonic cruise efficiency.

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Key concepts: Supersonic speed, Sonic boom, Cruise, Aerodynamics, Aerospace engineering, Aeronautics, Mach number, Engineering