Scramjet Isolator Shock-Train Leading-Edge Location Modeling-Reference-Cited by-同舟云学术

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Scramjet Isolator Shock-Train Leading-Edge Location Modeling

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Hutzel John¹,Decker Douglas¹,Donbar Jeffrey²

Affiliation:

1. Air Force Institute of Technology

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2223

Reference21 articles.

1. Scramjet Engines: The First Forty Years

2. Shock train and pseudo-shock phenomena in supersonic internal flows

3. Hypersonic Airbreathing Propulsion

4. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle

5. A Hypersonic Vehicle Model Developed With Piston Theory

Cited by 27 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. Flow field reconstruction and shock train leading edge position detection of scramjet isolation section based on a small amount of CFD data;Advances in Aerodynamics;2022-08-19

2. Locating the Isolator Shock-Train Leading Edge with Limited Pressure Information;Journal of Propulsion and Power;2021-11

3. Adaptive Pressure Profile Method to Locate the Isolator Shock Train Leading Edge Given Limited Pressure Information;AIAA Propulsion and Energy 2020 Forum;2020-08-17

4. Closed-Loop Control of Unstart in a Mach 1.8 Isolator;Journal of Propulsion and Power;2020-01

5. Closed-Loop Control of Unstart in a Mach 1.8 Isolator;AIAA Scitech 2019 Forum;2019-01-06

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