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Fire Detection Techniques for Supersonic Aircraft
ASME 1968 Gas Turbine Conference and Products Show, 1968The problems of detecting fire and overheat in a supersonic aircraft, while similar to those in subsonic aircraft, have certain unique characteristics. These characteristics are due basically to the dynamic and thermal environment associated with the Mach 3 to Mach 4.5 flight regime. This paper presents an approach toward the solution of these problems
G. T. Beery, T. M. Trumble
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Engines for Supersonic Civil Transport Aircraft
Aircraft Engineering and Aerospace Technology, 1961Because of its high overall pressure ratio and good propulsive efficiency, the jet engine is very efficient for supersonic propulsion. A high thrust per unit power plant frontal area and per unit weight are primary requirements and these imply high combustion temperatures. For a Mach 2.0 aircraft, engine design problems other than this are not outside
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Meteorological Requirements For Supersonic Transport Aircraft
1961This report outlines requirements for weather information for the supersonic transport intended to serve as a basis in the formulation, implementation and operation of an adequate weather support program.
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Charge Production, Supertankers and Supersonic Aircraft
Nature, 1972A RECENT series of explosions aboard supertankers during tank cleaning operations (using high pressure water jets) has raised the possibility that the sudden electrical discharge of an electrostatically charged mist may ignite an explosive mixture of hydrocarbon and air1. Although the discharge configuration (cloud–electrode) is somewhat different from
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Lubricants for Engines for Supersonic Aircraft
Aircraft Engineering and Aerospace Technology, 1962MOST of the aircraft engines of the 1900 era were little more than adaptations of the existing reciprocating internal combustion engines used in motor cars, but progressive design improvements eventually led to the very efficient power plants of high horsepower which had by the 1940's enabled piston‐engined bomber aircraft to reach cruising speeds of ...
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Drag Analysis of a Supersonic Fighter Aircraft
2016For aircraft design, drag optimization is very important for having better flight performance and less fuel consumption. In this study, drag effects of fuselage, wing and tail section are separately analyzed using a generic F-16 fighter aircraft model in ANSYS Fluent CFD tool with polyhedral mesh.
Kurtulus D. F. +3 more
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