Results 131 to 140 of about 431 (183)
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SAE Technical Paper Series, 1962
<div class="htmlview paragraph">Aircraft hydraulic systems have progressed from simple to complex, reliable systems, and in the future, with the Mach 3 aircraft, will be called upon to perform even more tasks. A review of past accomplishments, with a presentation of areas where progress is needed is examined in this paper.</div>
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<div class="htmlview paragraph">Aircraft hydraulic systems have progressed from simple to complex, reliable systems, and in the future, with the Mach 3 aircraft, will be called upon to perform even more tasks. A review of past accomplishments, with a presentation of areas where progress is needed is examined in this paper.</div>
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Supersonic Turbojet Noise Reduction
International Journal of Aeroacoustics, 2013Observations and Large Eddy Simulations are presented of a supersonic jet from a nozzle representative of high-performance military aircraft such as the Saab Gripen. The nozzle has a design Mach number of 1.56 and is examined at its design condition with a surrounding secondary flow at Mach numbers of 0.0, 0.1 and 0.3. The nozzle is investigated in its
David Munday +5 more
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Afterburners for Turbojet Engines
Journal of the Aeronautical Sciences, 1948The general problem of pure jet aircraft take-off distance is indicated, and the basic reasons for the excess-thrust deficiency as compared to propeller aircraft are shown. The inherent advantages and disadvantages of several methods of short-duration thrust augmentation, such as fluid injection or rocket boosters, to alleviate the difficulties are ...
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Noise From Turbojet Compressors
The Journal of the Royal Aeronautical Society, 1964SummaryThe noise radiated from the intakes of turbojet engines during landing is already causing a serious nuisance. This paper, which is largely based on the deliberations of an ad hoc working panel of academic experts formed by Rolls-Royce in 1961, describes the characteristics of the noise and discusses possible mechanisms of generation.
S. L. Bragg, R. Bridge
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Turbojet and Turboprop Engine Controls
SAE Technical Paper Series, 1951<div class="section abstract"><div class="htmlview paragraph">THE gas turbine fuel control situation is in a state of confusion, the author feels, because of such factors as the newness of gas turbine development, the lack of comparative evaluation tests on controls, and the lack of time for the results of field experience to become ...
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The Origins of the Turbojet Revolution
The American Historical Review, 1982Edward C. Ezell, Edward W. Constant
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Large Lightweight Turbojet Engines
SAE Technical Paper Series, 1958<div class="section abstract"><div class="htmlview paragraph">THIS paper deals with the general performance of turbojet engines in both subsonic and supersonic flight in relation to aircraft requirements.</div><div class="htmlview paragraph">The advantages and disadvantages of the bypass engine and small turbojet in relation to ...
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The Use of Ethanol as an Alternative Fuel for Small Turbojet Engines
Sustainability, 2021Rudolf Andoga +2 more
exaly