Experiment and numerical investigation of flow control on a supersonic inlet diffuser
Author:
Funder
National Natural Science Foundation
Jiangsu Province
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. US army hypersonic scramjet propelled missile technology program;Walker,2006
2. Hypersonic Airbreathing Propulsion;Heiser,1994
3. An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles;Ding;Acta Astronaut.,2018
4. Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers;Yue;Aerosp. Sci. Technol.,2018
5. Unstart/restart hysteresis characteristics analysis of an over-under TBCC inlet caused by backpressure and splitter;Li;Aerosp. Sci. Technol.,2018
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