Experimental research on the performance of the forward variable area bypass injector for variable cycle engines
Author:
Affiliation:
1. School of Energy and Power Engineering , Beihang University , No. 37 Xueyuan Road, Haidian District , Beijing , 100191, China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjeng-2020-0021/pdf
Reference21 articles.
1. Johnson, JE. Variable cycle engines the next step in propulsion evolution. 12th propulsion conference. Palo Alto, CA, US; 1976:0758. https://doi.org/10.2514/6.1976-758.
2. Krebs, J, Allan, RD. Supersonic propulsion-1970 to 1977. 13th propulsion conference. Orlando, FL, US; 1977:0832. https://doi.org/10.2514/6.1977-832.
3. Brown, RH. Integration of a variable cycle engine concept in a supersonic cruise aircraft. 14th joint propulsion conference. Las Vegas, NV, US; 1978:1049. https://doi.org/10.2514/6.1978-1049.
4. French, MW, Allen, GL. NASA VCE test bed engine aerodynamic performance characteristics and test results. 17th Joint Propulsion Conference. Colorado Springs, CO, US; 1981:1594. https://doi.org/10.2514/6.1981-1594.
5. Vdoviak, JW, Ebacher, JA. VCE test bed engine for supersonic cruise research. NASA. Langley Research Center Supersonic Cruise Res. 1979;1:347–56.
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1. Exploration of acceptable operating range for a compression system in a double bypass engine;Chinese Journal of Aeronautics;2023-09
2. Development and Validation of a Novel Control-Volume Model for the Injection Flow in a Variable Cycle Engine;Aerospace;2022-08-05
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