Injection studies in the French hypersonic technology program-Reference-Cited by-同舟云学术

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Injection studies in the French hypersonic technology program

Published:1995-04-03 Issue: Volume: Page:
ISSN:
Container-title:International Aerospace Planes and Hypersonics Technologies
language:
Short-container-title:

Author:

Scherrer D,Dessornes O,Ferrandon O,Monymayeur N

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-6096

Reference10 articles.

1. D. Scherrer, N. Montmayeur, 0. Ferrandon, D. Tonon AIAA 93-5171, Munich, Dcccmbcr 1993

2. Scramjet CombustorDesign inFrance M. Bouchez,N. Montmayeur. C.Lebouchei AlAA 95-6094,Chattanooga, 199.5

3. Imv Angle Injection Intoa Supersotiir Flow R.B. Mays, R.H. Thomas, J.A. Schetz AIAA 89-2461, 1989

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1. Thrust Control of Scramjet Based on BP Neural Network;Lecture Notes in Electrical Engineering;2024

2. Research progress on strut-equipped supersonic combustors for scramjet application;Progress in Aerospace Sciences;2018-11

3. Turbulent hypervelocity fuel/air mixing by cantilevered ramp injectors;10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference;2001-04-24

4. Mixing enhancement techniques in a scramjet;8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;1998-04-27

5. An industrial point of view on scramjet combustor design;Fluid Mechanics and Its Applications;1997

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