Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart
Author:
Affiliation:
1. University of Texas, Austin
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2808
Reference21 articles.
1. Hypersonic Airbreathing Propulsion
2. Experimental investigation of terminal shock sensors for mixed-compression inlets
3. Experimental Study of a Dual-Mode Scramjet Isolator
4. High-Frequency Pressure Measurements for Unstart Detection in Scramjet Isolators
5. Diode laser-based detection of combustor instabilities with application to a scramjet engine
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1. Robust Adaptive Control of Hypersonic Vehicle Considering Inlet Unstart;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2020-02
2. Control of pseudo-shock oscillation in scramjet inlet-isolator using periodical excitation;Acta Astronautica;2018-02
3. Mathematical Model of Shock-Train Path with Complex Background Waves;Journal of Propulsion and Power;2017-03
4. Transient Analysis for Hypersonic Inlet Accelerative Restarting Process;Journal of Spacecraft and Rockets;2017-03
5. A Computational Investigation of Unstart in a Dual-Mode Scramjet;54th AIAA Aerospace Sciences Meeting;2016-01-02
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