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Transonic drag characteristics and pressure distribution on the body of a wing-body combination consisting of a body of revolution of fineness ratio 12 and a wing having sweepback of 45 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoi

机译：翼体组合体上的跨音速阻力特性和压力分布由细度比为12的旋转体和具有45度后冲，纵横比4，锥度比0.6和NaCa 65a006气流的机翼组成。

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Kurbjun, Max C; Thompson, Jim Rogers;
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年度 1952
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. The Effect of Inboard and Outboard Wing Sweep Angles to Lift-to-Drag Ratio of a Compound Wing-Body Using Panel Code [J] . Rizal E. M. Nasir, Nabil F. Tajuddin, Atikah B. A. Mutaâ€™ali, Journal of Aeronautics Astronautics and Aviation . 2021,第2期

机译：舷内和外侧翼横扫角度利用面板代码剥离复合翼体的剥离比例
3. Control of Transonic Buffet by Shock Control Bumps on Wing-Body Configuration [J] . Mayer R., Lutz T., Kraemer E., Journal of Aircraft . 2019,第2期

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5. THEORETICAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A LIFTING, SUBSONIC DELTA WING OF ARBITRARY ASPECT RATIO. [D] . SWAIN, CARL EUGENE. 1971

机译：从理论上确定任意纵横比的提升亚音速三角翼上的压力分布。
6. Transcription phase protein characteristics of DEV UL45 and prokaryotic expression antibody preparation of the UL45 des-transmembrane domain [O] . Ai-Mei Shen, Guang-Peng Ma, An-Chun Cheng, 2010

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7. Some Effects of Taper Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Sweptback Angle of 45° and an Aspect Ratio 4.0 [O] . Eiichi NAKAI, Toshiro TAKAGI, Yasukatsu ANDO 1966

机译：锥形比对一系列薄悬臂机翼的横向振荡特性的一些效果，其具有45°的扫频角和纵横比4.0

Transonic drag characteristics and pressure distribution on the body of a wing-body combination consisting of a body of revolution of fineness ratio 12 and a wing having sweepback of 45 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoi

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