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A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow

机译：一种计算超音速流中小迎角机翼组合气动载荷的方法

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摘要

Theoretical method for calculating aerodynamic loading on wing-body combinations

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作者
Jackson, C. M., Jr.; Sawyer, W. C.;
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年度 1971
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; AERODYNAMIC LOADS; NUMERICAL ANALYSIS; WINGS; AERODYNAMIC STABILITY; MACH NUMBER; SUPERSONIC FLOW;

机译：空气动力学配置;空气动力负荷;数值分析; WINGs;空气动力学稳定性;马赫数;超音速流;
入库时间 2022-08-29 11:13:28

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6. A novel self-seeding method for particle image velocimetry measurements of subsonic and supersonic flows [O] . Omid Nematollahi, Hadi Samsam-Khayani, Mahdi Nili-Ahmadabadi, -1

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7. Aerodynamics of delta wing-body Combinations at high angles of attack - A project proposal [O] . Viswanath PR 1985

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8. A Method for Calculating the Aerodynamic Loading on Wing-Body Combinations at Small Angles of Attack in Supersonic Flow [R] . Jackson, C. M., Sawyer, W. C. 1971

机译：超音速小攻角下翼体组合气动载荷的计算方法

A method for calculating the aerodynamic loading on wing-body combinations at small angles of attack in supersonic flow

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