Side Jet Aerodynamic Interaction on a Blunt Body in Hypersonic Flow.
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/50/585/50_585_394/_pdf
Reference16 articles.
1. Mach 8 to 22 studies of flow separations due to deflected control surfaces
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3. 3) Hozumi, K., Yamamoto, Y., Fujii, K., Ledy, J. P., Devezeaux, D. and Fontaine, J.: Experimental Investigation of Hypersonic Aerodynamic Heating on Compression Ramp at High Angles of Attack, AIAA Paper 2000-2597, 2000.
4. Sidejet Aerodynamic Interaction Effects of the Missile
5. Experimental investigation of side-jet steering for supersonic and hypersonic missiles
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1. Three-Dimensional Hypersonic Aeroheating Computations Associated with Cross-Flow Jet Interactions;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2020
2. Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow;International Journal of Aerospace Engineering;2017
3. The Role of Vortices in Side Jet/Blunt Body Interaction at Hypersonic Speed;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN;2009
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