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- W345166262 abstract "Abstract : A conceptual design study has been completed to investigate the application of advanced technologies in a low cost experimental fighter that could double the cruise speed of current and emerging fighters. Conceptual design studies were conducted with USAF/AFFDL sponsorship under Contract F33615- 75-C-3150. Wind tunnel tests were conducted under a Boeing indepedent research program to verify performance results. The Light Experimental Supercruiser concept employs six major technologies: (1) Advanced supersonic aerodynamics, (2) Variable Camber Wing Geometry, (3) Low Profile cockpit, (4) Damage tolerant composite structure, (5) Digital fiber-optic flight controls, and (6) Two- Dimensional Airframe Integrated Exhaust System. The air vehicle design is based on NASA SCAT 15 arrow wing research and is powered by a modified General Electric J101 engine." @default.
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- W345166262 date "1976-07-01" @default.
- W345166262 modified "2023-09-26" @default.
- W345166262 title "Light Experimental Supercruiser Conceptual Design" @default.
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