Plasma Flow Control of Non-bistable Vortex Pair over a Slender Conical Forebody
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_77
Reference17 articles.
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3. Mcelroy C, Sharp P (1971) An approach to stall/spin development and test. In: AIAA Paper, 71-772 (1971)
4. Stinton D (2001) The Design of the Airplane. Second Edition (General Publication) 2nd Edition. American Institute of Aeronaut
5. Keener E, Chapman G, Taleghani J, Chohen L (1977) Side forces on forebodies at high angle of attack and Mach numbers from 0.1 to 0.7: two tangent ogives paraboloid and cone. NASA TM X-3438
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