Results 221 to 230 of about 14,411 (284)
Preliminary Altitude Performance Data of J71-A2 Turbojet Engine Afterburner
, 1954 James W Useller, William E. Mallett
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2021
Dr. Kollmann (and his colleagues) were keenly aware that the jet engine was the powerplant of future. They clearly stated this when interrogated by the British intelligence agents in June 1945 (from Report POW/ENG/6, Evaluation Report No. 539, 16 Apr 46).
Karl Kollmann +2 more
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Dr. Kollmann (and his colleagues) were keenly aware that the jet engine was the powerplant of future. They clearly stated this when interrogated by the British intelligence agents in June 1945 (from Report POW/ENG/6, Evaluation Report No. 539, 16 Apr 46).
Karl Kollmann +2 more
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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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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.
David Munday +5 more
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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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Biofueled Miniature Turbojet Engine (BIOMITE)
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012The Busemann Advanced Concepts Lab at the University of Colorado Boulder has been researching improvements to small turbojet engines designed for unmanned aerial vehicles for the past three years. The BIOMITE senior design team has continued this tradition by designing adaptations for a commercial-off-the-shelf US Microjet AT-450 turbojet engine to run
Gregory Rancourt +2 more
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Greenization Factor of a Turbojet Engine
2017[No abstract available]
Şöhret, Yasin, Karakoç, Tahir Hikmet
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Turbojet Engine Simulation Using Dymola
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006This work describes the development of a global model of a modified turbojet engine for dynamic behavior simulation. The Modelica language is used for the simulation of this model. A Modelica package was created for the basic components suitable for such models. The model is based on a general turbojet engine and a turbofan engine. The engine component
Jiwu Shen +2 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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