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Effects of Forebody Geometry on the Flow and Control of a Blunt- Nose Projectile at High Angles of Attack

机译：前体几何形状对高攻角钝嘴弹丸流动和控制的影响

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《AIAA Aerospace Sciences Meeting and Exhibit》|2007年|P.1-31|共31页
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J. Lopera; T. Ng; M. Patel;
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中图分类航空;
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2. Plasma flow control over forebody at high angles of attack [J] . Zhao Z., Gao C., Liu F., Modern Physics Letters, B. Condensed Matter Physics, Statistical Physics, Applied Physics . 2010,第13期

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3. Forebody Flow Control for Extended High-Angle-of-Attack Maneuvers [J] . F. Hodgkin, N. J. Wood Journal of Aircraft . 1998,第2期

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4. Effects of Forebody Geometry on the Flow and Control of a Blunt- Nose Projectile at High Angles of Attack [C] . AIAA Aerospace Sciences Meeting and Exhibit . 2007

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5. High angle of attack: Forebody flow physics and design emphasizing directional stability. [D] . Ravi, R. 1998

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7. Effects of Forebody Geometry on Side Forces on a Cylindrical Afterbody at High Angles of Attack [O] . Serdaroglu Timucin, Pahlavani Hamed, Ozdemir I Bedii 2020

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8. Experimental investigation of the effects of aft blowing with various nozzle exit geometries on a 3.0 caliber tangent ogive at high angles of attack: Forebody pressure distributions [R] . Chokani, Ndaona, Gittner, N. M. 1992

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Effects of Forebody Geometry on the Flow and Control of a Blunt- Nose Projectile at High Angles of Attack

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