Real-time online unstart prediction of supersonic inlet based on pressure fluctuations
Author:
Funder
Fundamental Research Funds for the Central Universities
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference33 articles.
1. Starting characteristics of supersonic inlets;Van Wie,1996
2. Unstart phenomena induced by flow choking in scramjet inlet-isolators;Im;Prog. Aerosp. Sci.,2018
3. Recent research progress on unstart mechanism, detection and control of hypersonic inlet;Chang;Prog. Aerosp. Sci.,2017
4. Oscillatory flows of rectangular hypersonic inlet unstart caused by downstream mass-flow choking;Tan;J. Propuls. Power,2009
5. CIAM/NASA Mach 6.5 scramjet flight and ground test;Voland,1999
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