Results 201 to 210 of about 31,952 (223)
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Engineering Aspects of Supersonic Aircraft
Nature, 1963Supersonic Engineering A Symposium held at the Royal College of Advanced Technology, Salford. Edited by J. T. Henshaw. Pp. viii + 264. (London: William Heinemann, 1962.) 63s.
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Supersonic Aircraft Shape Optimization
1997This paper will discuss examples of supersonic aerodynamic shape optimization as developed for Daimler-Benz Aerospace Airbus by Synaps, Inc.
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The Airworthiness of Supersonic Aircraft
Aircraft Engineering and Aerospace Technology, 1969IF the history of air transport is traced back we find that superimposed on a steady rate of development, there have been several important milestones standing out as major jumps in technological progress. The first cabin airliner‐the first monoplane‐the first pressure cabin‐the first turbine‐the first jet and now the first supersonic transport.
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Study of Unmanned Supersonic Aircraft Configuration
SAE Technical Paper Series, 2014<div class="section abstract"><div class="htmlview paragraph">The aim of this work is to present the preliminary performance studies of the unmanned, lightweight (less than 10 kg), supersonic research aircraft. The studies comprise the typical mission for the aircraft's first supersonic version, based on the aerodynamic, thrust, and mass ...
Luciano Magno Frágola Barbosa +2 more
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Exhaust Nozzles For Supersonic Aircraft
The Journal of the Royal Aeronautical Society, 1958The Ordinary convergent exhaust nozzle is a perfectly satisfactory and efficient device for converting pressure in the jet pipe into velocity, so long as the pressure ratio across it remains below about 2.0; or, put another way, so long as the velocity at exit from the nozzle is not theoretically greater than that of sound at the jet temperature ...
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Supersonic Aircraft—Promise and Problems
The Journal of the Royal Aeronautical Society, 1960The 1,157th lecture to be given before the Society, “Supersonic Aircraft—Promise and Problems” by M. B. Morgan, Esq., C.B., M.A., F.R.Ae.S., Scientific Adviser to the Air Ministry, was given on 17th March 1960, at the Institution of Mechanical Engineers. Mr. Peter G.
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SUPERSONIC AIRCRAFT BRING LUBRICATION PROBLEMS
Industrial Lubrication and Tribology, 1968THE ATTENTION which has been paid in both the lay and technical press to the Concorde has revealed the many problems associated with the design and construction of aircraft flying at supersonic speeds. They relate to both aerodynamic design and the materials of construction where, particularly for the latter, one of the main influencing factors is the ...
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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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