Computational Analysis of Flow Phenomena in a Back-Pressured Supersonic Isolator
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4762
Reference22 articles.
1. The effect of aspect ratio on isolator performance
2. Understanding Isolator Performance Operating in the Separation-Shock Mode
3. Oscillation Phenomena of Pseudo-Shock Waves
4. TDLAS-based Measurements of Temperature, Pressure, and Velocity in the Isolator of an Axisymmetric Scramjet
5. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking
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1. Pressure Effects in a Scramjet Combustor;AIAA Propulsion and Energy 2021 Forum;2021-07-28
2. The Effects of Isolator Length on Combustion in a Scramjet Engine Model;AIAA Propulsion and Energy 2020 Forum;2020-08-17
3. Distinguishing Characteristics of Thermally- and Mechanically-Generated Backpressure;AIAA Scitech 2019 Forum;2019-01-06
4. On the Backpressure Phenomenon in Modeled Dual-Mode Scramjets;2018 Joint Propulsion Conference;2018-07-08
5. Studies on Leading Edge Detection in Mechanically- and Combustion-Generated Shock Trains in Dual-Mode Scramjet Engines;55th AIAA Aerospace Sciences Meeting;2017-01-05
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