An Experimental Investigation to Use the Biodiesel Resulting from Recycled Sunflower Oil, and Sunflower Oil with Palm Oil as Fuels for Aviation Turbo-Engines. [PDF]
Int J Environ Res Public Health, 2021 Cican G +4 more
europepmc +1 more source
Review of ejector nozzles. Part 2 – Mixers and additional information
Авіаційно-космічна техніка та технологіяThe subject of this article is ejector nozzles, which are intended for the thrust augmentation of jet engines and their corresponding flow mixers. The goal is to soften the acuteness of contradictions between the required high performance (especially ...
Ruslan Tsukanov, Sergiy Yepifanov
doaj +1 more source
Assessment of a regulatory measurement system for the determination of the non-volatile particulate matter emissions from commercial aircraft engines. [PDF]
J Aerosol Sci, 2021 Kinsey JS +27 more
europepmc +1 more source
Flight velocity effects on exhaust noise of a wedge nozzle installed on an underwing nacelle on an F-106 airplane [PDF]
It is important to know whether the relatively high takeoff speeds of supersonic transport aircraft will change the exhaust noise levels of nozzles from those measured at static conditions.
Burley, R. R.
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Aeronautical Engineering: A special bibliography with indexes, supplement 64, December 1975 [PDF]
This bibliography lists 288 reports, articles, and other documents introduced into the NASA scientific and technical information system in November ...
core +1 more source
Three-Dimensional Computational Fluid Dynamics Simulation of the Turbine Blades of a Micro Turbojet Engine [PDF]
, 2023 Haotian Zhang
openalex +1 more source
Combined Methods in Preliminary Micro Scale Gas Turbine Diffuser Design – a Practical Approach
Journal of Applied Fluid Mechanics, 2018 Micro scale gas turbines are low cost, simplified versions of full scale jet engines. A unique feature of their design are centrifugal compressor impellers that are selected from automotive low cost, high quality turbocharger components.
M. Czarnecki, J. Olsen
doaj
Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler. [PDF]
Micromachines (Basel), 2022 Zhang J, Zou Z, Wang Y.
europepmc +1 more source
On the use of relative velocity exponents for jet engine exhaust noise [PDF]
The effect of flight on jet engine exhaust noise has often been presented in terms of a relative velocity exponent, n, as a function of radiation angle.
Stone, J. R.
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Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [PDF]
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital computer is presented. The method involves linearization of nonlinear dynamic equations about an operating point on a speed line, and then application of ...
Blaha, R. J. +2 more
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