Numerical modeling on installed performance of turbofan engine with inlet ejector
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference40 articles.
1. Investigation on incompressible lobed mixer-ejector performance;Shan;J. Propuls. Power,2015
2. Aircraft powerplant and plume infrared signature modelling and analysis;Rao,2005
3. Numerical modeling on pumping performance of piccolo-tube multi-nozzles supersonic ejector in an oil radiator passage;Shan;Energy,2018
4. Numerical investigation on the effect of nozzle position for design of high performance ejector;Zhang;Appl. Therm. Eng.,2017
5. Numerical investigation on the mixing process in a steam ejector with different nozzle structures;Yang;Int. J. Therm. Sci.,2012
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