Results 101 to 110 of about 19,118 (298)
Compressor noise analysis [PDF]
Prediction method for noise radiation from turbojet compressor ...
Lowson, M. V.
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Unsteady flow characteristic analysis of turbine based combined cycle (TBCC) inlet mode transition
Propulsion and Power Research, 2015 A turbine based combined cycle (TBCC) propulsion system uses a turbine-based engine to accelerate the vehicle from takeoff to the mode transition flight condition, at which point, the propulsion system performs a “mode transition” from the turbine to ...
Jun Liu, Huacheng Yuan, Guo Rongwei
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Closure to “Discussion of ‘Characteristics of Turbojet Engines at High Flight Speeds’” (1947, Trans. ASME, 69, p. 243) [PDF]
, 1947 C. A. Meyer
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A turbojet-boosted two-stage-to-orbit space transportation system design study [PDF]
The concept to use twin turbo-powered boosters for acceleration to supersonic staging speed followed by an all rocket powered orbiter stage was proposed. A follow-on design study was then made of the concept with the performance objective of placing a 29,
Hepler, A. K. +3 more
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Medium independent jet (MI-Jet) engine
Propulsion and Power Research, 2020 MI-Jet or medium independent jet engine is a new conceptual design which can be used in any gaseous atmosphere or in any planets with an ISP greater than that of the existing rocket engines.
Prajith Kumar K P, Aravind Vaidyanathan
doaj
Optimized modeling of energy and environmental metrics of mixed flow turbofan engine used regional aircraft. [PDF]
J Therm Anal Calorim, 2023 Uçar UU, Aygun H, Tanyeri B.
europepmc +1 more source
International Journal of Environmental Science and Technology, 2018 It is forecast that in the future, alternative fuels derived from non-petroleum sources will become the basic propellant for turbine aircraft engines. Currently, five types of aviation turbine fuel containing synthesized hydrocarbons are certified and ...
B. Gawron, T. Białecki
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Energy-Effective Rotation Equipment
Известия высших учебных заведений и энергетических объединенний СНГ: Энергетика, 2013 The article presents invention, which allows to create compact and cheap fog-forming devices for industrial hothouses (plants), greenhouses, storehouses, testing polygons and other Objects. Besides, this invention gives the possibilities to modernize the
V. G. Kascheev +5 more
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Development of a turbojet combustor with a segmentally constructed liner Final summary report [PDF]
Axial and circumferential segmented combustor liners for turbojet ...
Biondi, D., Draizen, S.
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