Aerodynamic performance enhancement of a variable-geometry dual-mode combustor designed by the method of characteristics-Reference-Cited by-同舟云学术

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Aerodynamic performance enhancement of a variable-geometry dual-mode combustor designed by the method of characteristics

Published:2021-01 Issue: Volume:108 Page:106353
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Youyin^ORCID,Shi Wen,Wang Xuan,Zhang Junlong,Gao Jin^ORCID,Tang Jingfeng,Chang Juntao,Bao Wen^ORCID

Funder

China National Natural Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference47 articles.

1. History of U.S. navy ramjet, scramjet, and mixed-cycle propulsion development;Waltrup;J. Propuls. Power,2002

2. Experimental investigation of a three-dimensional scramjet engine at Mach 12;Wise,2015

3. Mixing and combustion control strategies for efficient scramjet operation in wide range of flight Mach number;Sunami,2002

4. French-Russian partnership on hypersonic wide-range ramjets;Bouchez Fran-atilde;J. Propuls. Power,2001

5. Transverse jet in supersonic crossflows;Huang;Aerosp. Sci. Technol.,2016

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1. Extended-Kalman-filter-based equilibrium manifold expansion observer for ramjet nonlinear control;Aerospace Science and Technology;2023-07

2. Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor;Energy;2022-12

3. Behaviors of the long penetration mode with a hot counterflowing jet;Aerospace Science and Technology;2022-11

4. Numerical Investigation on Performance of Axisymmetric Variable Geometry Scramjet Combustor Equipped with Strut Flame Holder;Combustion Science and Technology;2021-10-08

5. Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling;Aerospace Science and Technology;2021-10

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