Numerical Experiments of Scramjet Combustion with Boundary-Layer Bleeding-Reference-Cited by-同舟云学术

Numerical Experiments of Scramjet Combustion with Boundary-Layer Bleeding

Published:2003-12-15 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA International Space Planes and Hypersonic Systems and Technologies
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Author:

Kouchi Toshinori,Mitani Tohru,Kodera Masatoshi,Masuya Goro

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-7038

Reference20 articles.

1. Sakuranake, N., Tomioka, S., Izumikawa, M., and Mitani, T. "Boundary Layer Bleeding Device for Scramjet Engines," Proceedings of the 4th Symposium on Propulsion System for Reusable Launch Vehicles, pp.209-214, 2003(inJapanese)

2. Numerical analysis of scramjet combusting flows by unstructured hybrid grid method

3. Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility

4. Hiraiwa, T., Kobayashi, K., Wakamatsu, Y., Mitani, T. "Heat Flux on Scramjet Engine at Mach 4 Flight Condition and Heat Flux Meter Evaluation," Proceedingsofthe4thSymposiumonPropulsion SystemforReusableLaunchVehicles,pp.197-202, 2003(inJapanese)

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