Development of Methods to Predict High-Speed Reacting Flows in Aerospace Propulsion Systems-Reference-Cited by-同舟云学术

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Development of Methods to Predict High-Speed Reacting Flows in Aerospace Propulsion Systems

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Drummond J. Philip¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-112

Reference160 articles.

1. 2Digger,D.L.“ComparisonofHypersonicRamjetEngineswithSubsonicandSupersonicCombustion,”ProceedingsoftheFourthAGARD Colloquium,AGARD,1960.

2. 3Northam,G.B.andAnderson,G.Y.“LinearStabilityAnalysisofDensityStratifiedParallelShearFlows,”AIAAPaper86-0159,1986.

3. Evolution and application of CFD techniques for scramjet engine analysis

4. 5Walthrup,P.J.andBillig,F.S.“LiquidFueledSupersonicCombustionRamjets;AResearchPerspectiveofthePast,Present,andFuture,” AIAAPaper86-0158,1986.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. LES investigation of nonequilibrium flow in a cavity-flameholding axisymmetric scramjet;AIAA Propulsion and Energy 2021 Forum;2021-07-28

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