T6: The Oxford University Stalker Tunnel-Reference-Cited by-同舟云学术

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T6: The Oxford University Stalker Tunnel

Published:2015-07-02 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

McGilvray Matthew,Doherty Luke J.,Morgan Richard G.,Gildfind David,Jacobs Peter,Ireland Peter

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3545

Reference25 articles.

1. 1Fletcher, D. G. “Fundamentals of Hypersonic Flow - Aerothermodynamics,” Tech. Rep. RTO-EN-AVT-116, NATO,2004, RO AVT Lecture Series.

2. The production of pulsed nozzle flows in a shock tube

3. Wave processes in scramjet thrust generation

4. Design and Test of a Hypersonic Isentropic-Spike Intake with Aligned Cowl

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2. Combustion of High-Pressure Hydrogen Diluted Mixtures in ESTHER Shock Tube;Journal of Thermophysics and Heat Transfer;2024-07-01

3. An Improved Model of Free Piston Compressor Considering Entropy Change;Lecture Notes in Electrical Engineering;2024

4. Study of Radiation Characteristics of Shock-Heated Gases;Journal of Engineering Physics and Thermophysics;2023-11

5. Numerical simulation of transpiration cooling for a high-speed boundary layer undergoing transition to turbulence;Aerospace Science and Technology;2023-10

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