Computational Prediction of Nose- Down Control for the Pre- Production F/A- 18E at High Angles of Attack

机译：预生产的F / A-18E高攻角时机头下降控制的计算预测

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《AIAA Guidance, Navigation and Control Conference and Exhibit; AIAA Atmospheric Flight Mechanics Conference and Exhibit; AIAA Modeling and Simulation Technologies Conference and Exhibit》|2007年|P.1-15|共15页
会议地点 Hilton Head SC(US);Hilton Head SC(US);Hilton Head SC(US)
作者
B. Green;
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作者单位

Naval Air Systems Command, Patuxent River, MD;

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会议组织
原文格式 PDF
正文语种
中图分类飞行控制系统与导航;
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1. Computational challenges in high angle of attack flow prediction [J] . Russell M. Cummings, James R. Forsythe, Scott A. Morton, Progress in Aerospace Sciences . 2003,第5期

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2. How to extract the angle attack on airfoils in cycloidal motion from a flow field solved with computational fluid dynamics? Development and verification of a robust computational procedure [J] . Melani Pier Francesco, Balduzzi Francesco, Ferrara Giovanni, Energy Conversion & Management . 2020,第Nova期

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3. Investigation of the effects of angle of attack and tail deflection angle on the controlling tail flow field [J] . Ali Mokhtari, Azadeh Shahrian, Pooya Javadpoor Langroodi, Aerospace Systems . 2020,第4期

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4. Computational Prediction of Nose- Down Control for the Pre- Production F/A- 18E at High Angles of Attack [C] . B. Green AIAA Atmospheric Flight Mechanics Conference and Exhibit . 2007

机译：预生产的F / A-18E在大迎角下机头下降控制的计算预测
5. An experimental investigation of the physical mechanisms controlling the asymmetric flow past slender bodies at large angles of attack. [D] . Moskovitz, Cary A. 1989

机译：实验研究了在大迎角下控制不对称流动通过细长体的物理机制。
6. Myofiber angle distributions in the ovine left ventricle do not conform to computationally optimized predictions [O] . Daniel B. Ennis, Tom C. Nguyen, Jonathan C. Riboh, -1

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7. Stall-delay prediction at high angle of attack on wind turbine blade using computational fluid dynamics [O] . กัมพล อรนนท์ 2556

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8. Pitch Control Margin at High Angle of Attack-Quantitative Requirements (FlightTest Correlation with Simulation Predictions) [R] . Lackey, J., Hadfield, C. 1992

机译：高攻角下的俯仰控制余量 - 定量要求（FlightTest与模拟预测的相关性）

Computational Prediction of Nose- Down Control for the Pre- Production F/A- 18E at High Angles of Attack

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