Analysis of Limitations Imposed on One-Spool Turbojet-Engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers [PDF]
Limitations on turbojet engine design by turbines with downstream ...
Cavicchi, R. H., Constantine, A. B.
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Correlation of Turbojet Noise with Engine Design [PDF]
The Journal of the Acoustical Society of America, 1955 The dependence of the total acoustic power radiated by a turbojet engine on one dimensionless parameter was put forward by Mawardi and Dyer. This relationship is reviewed in the light of further data, and also the dependence of acoustic power on a number of other parameters, dimensionless and otherwise, is presented.
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Discussion: “The MU-CYL-JET: The Multicylinder Turbojet Engine” (Pinnes, R. W., 1962, ASME J. Eng. Power, 84, pp. 131–137) [PDF]
, 1962 Ernest C. Simpson
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Nuclear JT11D-20 Turbojet Engine Estimated Performance 1800F NaK Radiator
, 1960 J. W. Larson
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Photographic data on the influence of the composition, preparation method, time and fuel system on the size of water droplets in a fuel-water emulsion. [PDF]
Data Brief, 2022 Niszczota P, Gieras M.
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NSEG, a segmented mission analysis program for low and high speed aircraft. Volume 1: Theoretical development [PDF]
A rapid mission analysis code based on the use of approximate flight path equations of motion is presented. Equation form varies with the segment type, for example, accelerations, climbs, cruises, descents, and decelerations.
Hague, D. S., Rozendaal, H. L.
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Closure to “Discussions of ‘A Rotating Stall Control System for Turbojet Engines’” (1979, ASME J. Eng. Power, 101, pp. 313–314) [PDF]
, 1979 G. R. Ludwig, J. P. Nenni
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The influence of dynamic factors on the characteristics of the aviation engine in operating modes
Авіаційно-космічна техніка та технологіяIn the range of different flow modes for selecting the dimensions of the flow part, the rotor rotation frequency, and the design of compressors and turbines, the highest tension values for the strength were considered.
Serhii Tovkach
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Discussion: “A Rotating Stall Control System for Turbojet Engines” (Ludwig, G. R., and Nenni, J. P., 1979, ASME J. Eng. Power, 101, pp. 305–313) [PDF]
, 1979 STEPHEN ARNETT
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Combustor Design for Turbocharger Turbojet Engine
, 2016 This research explains several variation designs of the combustion chamber for a turbojet engine based of T70 turbocharger. T70 turbocharger engines are widely used in vehicles, especially cars. The problem that often occurs in the combustion chamber is the non-uniform flow which makes a pressure loss.
Fuad, N. +2 more
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