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Analysis of PIV Results Obtained for the VFE- 2 65?° Delta Wing Configuration at Sub- and Transonic Speeds

机译：VFE-2 65？°三角翼配置在亚音速和跨音速下获得的PIV结果分析

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来源
《24th Applied Aerodynamics Conference》|2006年|P.1-15|共15页
会议地点 San Francisco CA(US)
作者
R. Konrath; A. Schr?;
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作者单位

DLR German Aerospace Research Center, G??ttingen, Germany;

?der and J. Kompenhans, DLR German Aerospace Center, G??ttingen, Germany;

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会议组织
原文格式 PDF
正文语种
中图分类空气动力学;
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3. Influence of Stores on the Transonic Flutter of a Delta Wing Configuration [J] . Hiroshi Terashima, Kozo Fujii AIAA Journal . 2007,第1期

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4. Analysis of PIV Results Obtained for the VFE- 2 65?° Delta Wing Configuration at Sub- and Transonic Speeds [C] . Applied Aerodynamics Conference . 2006

机译：在跨音速度下对VFE-2 65的PIV结果分析PIV结果
5. Modeling the rolling moment on the 65-degree delta wing for rolling motions at high angle of attack. [D] . Myatt, James Harold. 1997

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6. Aerodynamics of a highly irregular body at transonic speeds—Analysis of STRATOS flight data [O] . Markus Guerster, Ulrich Walter 2011

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7. Transonic perturbation analysis of wing-fuselage-nacelle-pylon configurations with powered jet exhausts [O] . Wai, J. C., Sun, C. C., Yoshihara, H. 1982

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机译：兰格利8速高速隧道在高次谐波机械数量和1.2的机械数量下的跨音速调查分析具有45°扫描翼的纵向配置的压力分布，宽高比4，锥度比0.6 ，aND-NaCa 65a006翼型部分

Analysis of PIV Results Obtained for the VFE- 2 65?° Delta Wing Configuration at Sub- and Transonic Speeds

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