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Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations. [PDF]

Entropy (Basel)
Li C, Zhao W, Liu H, Xue Y, Yang Y, Chen W.   +5 more
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Supersonic Aircraft Energy Turns

IFAC Proceedings Volumes, 1972
Abstract A brief review is given of some recent theoretical work on optimal atmospheric flight, comprising an extension of so-called “energy climbs” to three-dimensional flight and an analytical recasting in terms of singular perturbation theory. A family of variable-altitude turns obtained by numerical integration in the reduced-order (“energy ...
Henry J. Kelley, Leon Lefton
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The Airworthiness of Supersonic Aircraft

The Aeronautical Journal, 1967
SummaryThe safety target for the Supersonic Transport has been set by the governments sponsoring the project. This is to achieve a safety level at least as good as that of subsonic aircraft at the same time. An analysis of present accident trends is used to give more precision to this statement.
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Arrow Wings for Supersonic Cruise Aircraft

Journal of Aircraft, 1978
The arrow wing planform has a far greater range potential than the delta wing planform for utilization on a commercial supersonic cruise vehicle. A supersonic cruise vehicle concept must be configured to favor cruise efficiency. The arrow wing planform cruise lift-drag ratio is approximately one unit higher than the delta wing.
B. WRIGHT, F. BRUCKMAN, N. RADOVCICH
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Noise from Aircraft at Supersonic Speeds

Nature, 1953
THE acoustic phenomena accompanying the dive of an aircraft to attain supersonic speed appear to be adequately explained by the Huyghens wavelet construction. The case of a body moving at a uniform supersonic speed V in a straight path, in a uniform atmosphere, is well known.
C H E, WARREN, E W, BASTIN, P, ROTHWELL
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Wing platforms of supersonic aircraft

Práce a štúdie, 2023
Goal of the paper is to describe various wing designs used in supersonic aircraft and their impact on lift, drag and stability with emphasis on high speed civil transport. Paper describes transonic and supersonic region, where formation of shockwaves is prevalent, and air behaves differently from subsonic region. The paper then describes different wing
Richard Tabernaus, Martin Bugaj, Michal Hrúz   +2 more
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Supersonic and Transonic Aircraft Problems

Journal of the American Rocket Society, 1947
A great honor has been conferred on me, especially the invitation^which said that I was particularly qualified" to discuss supersonic and transonic aircraft problems. Throughout my ! disertation the emphasis is going to be placed entirely on that word 'problem'. As so ably put by General Craigie quite recently in that "with respect to many of the major
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Extensions to aircraft pre-design for supersonic aircraft

52nd Aerospace Sciences Meeting, 2014
Forecasts predict a strong market for supersonic travel in the business sector. It is especially appealing for high-net-worth individuals because of both, the reduction of travel time and prestige. The ecological and economic challenges that are related to supersonic flight need adequate answers in terms of technology and tools to assess aircraft ...
Martin Schuermann, Peter Horst, Michele Gaffuri   +2 more
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Supersonic Transport Aircraft

Aircraft Engineering and Aerospace Technology, 1961
Arguments in favour of selecting a cruising speed of about M=2.0 for a long‐range supersonic transport aircraft have been given by Morgan, and Kuchemann has shown that the slender wing shapes provide the basis for the layout of the aircraft, and has given the general properties which would lead to the achievement of optimum cruising lift‐drag ratios ...
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