Supersonic ground vehicle

Aeronautics and astronautics – Aircraft sustentation

Patent

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Details

244 2, 244 36, 244200, 244117R, 244119, 244130, B64C 100

Patent

active

060562382

ABSTRACT:
A supersonic ground vehicle having a housing configured from a pair of back-to-back symmetric housing components, and a shock-reflecting surface which extends in the direction of travel of the housing and which aerodynamically interacts with the housing to form a supersonic biplane, thereby substantially reducing aerodynamic pressure drag.

REFERENCES:
patent: 934771 (1909-09-01), Turnbull
patent: 2136403 (1938-11-01), Vance et al.
patent: 2649266 (1953-08-01), Darrieus
patent: 3249327 (1966-05-01), Smith, Jr.
patent: 4735381 (1988-04-01), Wood
patent: 5372332 (1994-12-01), Spacht et al.
patent: 5395072 (1995-03-01), Nelson
Ascher H. Shapiro, "The Dynamics and Thermodynamics of Compressible Fluid Flow", vol. I, pp. 579-580. date unknown.
H.W. Liepmann and A. Roshko, "Elements of Gasdynamics", pp. 115-118. date unkown.
A. Busemann, "Aerodynamischer Auftrieb Bei Uberschallgeschwindigkeit", Atti del Convengo della Fondazione Alessandro Volta 1935, pp. 328-360 (1936). month unknown.
NACA TN 3183 "Minimum Wave Drag Airfoil Sections for Arrow Wings" May 1954.
Eggers, Jr. Some Considerations of Aircraft Configurations Suitable for Long-Range Supersonic Vehicle.
NACA 1211 The Flow and Force Characteristics of Supersonic Airfoils at High Supersonic Speeds date unknown.

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