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Wing-body interference at supersonic speeds with an application to combinations with rectangular wings

机译：超音速下的机翼干涉，适用于矩形机翼的组合

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Nielsen, Jack N; Pitts, William C;
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年度 1952
页码 1-67
总页数 67
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. VALIDATION OF PARAS3D RANS PRESSURE DATA WITH FLIGHT RESULTS OVER A WING-BODY RLV CONFIGURATION AT SUPERSONIC HIGH ANGLE OF ATTACK CONDITIONS [J] . G. Vidya, K. Manokaran, C. Babu, Journal of Aerospace Sciences and Technologies . 2019,第1期

机译：超音速攻击条件下机翼RLV构型上飞行结果的PARAS3D雷达压力数据验证
2. Robust Design of a Supersonic Natural Laminar Flow Wing-Body [J] . Domenico Quagliarella, Emiliano Iuliano IEEE computational intelligence magazine . 2017,第4期

机译：超音速自然层流机翼的稳健设计
3. Supersonic Wing-Body Two-Level Wave Drag Optimization Using Extended Far-Field Composite-Element Methodology [J] . Xiaohui Guan AIAA Journal . 2014,第5期

机译：使用扩展远场复合元素方法的超音速机翼两级波阻力优化
4. Favorable in interference of optimized wing-body combination with inlets at supersonic speed [C] . Dr.T.M.Pritulo, Dr.A.A.Gubanov, Dr.N.V.Voevodenko 1st AIAA Aircraft Engineering, Technology, and Operations Congress September 19-21, 1995/Los Angeles, CA . -1

机译：有利于优化的机体组合与超音速进气口的干扰
5. Rolling moment response of a wing-body to stagnation point actuation. [D] . Darden, Leigh-Ann. 1997

机译：机翼机体对停滞点致动的侧倾响应。
6. First Approximation of Pressure Distribution on Curved Profiles at Supersonic Speeds [O] . T. Y. Thomas 1949

机译：超音速下曲线轮廓上压力分布的第一近似
7. Supersonic wing-body interference [O] . Nielsen Jack Norman 1951

机译：超音速翼身干扰
8. Wing-Body Interference at Supersonic Speeds With an Application to Combinations With Rectangular Wings [R] . Nielsen, J. N., Pitts, W. C. 1952

机译：超音速下的机体干涉与矩形翼组合的应用

Wing-body interference at supersonic speeds with an application to combinations with rectangular wings

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