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An experimental investigation of the effect of Reynolds number on the low speed aerodynamic characteristics of a delta wing space shuttle orbiter concept at angles of attack to 45 degrees

机译：雷诺数对三角翼航天飞机轨道器概念在45度迎角下低速气动特性影响的实验研究

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作者
Parrell, H.;
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年度 1971
页码 1-306
总页数 306
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ANGLE OF ATTACK; DELTA WINGS; LOW SPEED; REYNOLDS NUMBER; SPACE SHUTTLES; BOUNDARY LAYER SEPARATION; GRAPHS (CHARTS); LATERAL STABILITY; WING TIPS;

机译：攻击角度; DELTa WINGs;低速; REYNOLDs NUmBER;太空沙滩;边界层分离;图表（图表）;横向稳定性; WING TIps;

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专利

1. A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST [J] . Makoto Kamishita, Shigeru Aso, Yuichi Kumamoto 九州大学工学集報 . 1997,第5期

机译：低速达达机翼大迎角空气动力学特性研究以开发下一代SST
2. Aerodynamic Characteristics of a Delta Wing in the Case of Harmonic Oscillations with Respect to the Roll and Yaw Angles at High Angles of Attack [J] . E. A. Karavaev, E. A. Chasovnikov Fluid Dynamics . 2013,第2期

机译：相对于大迎角的侧倾角和横摆角，在谐波振荡情况下三角翼的空气动力学特性
3. Effect of vortex shedding in unsteady aerodynamic forces for a low Reynolds number stationary wing at low angle of attack [J] . Villegas A., Diez F. J. Journal of Fluids and Structures . 2016,第Null期

机译：低雷诺数低攻角固定涡旋在非定常空气动力中涡流脱落的影响
4. Low Reynolds number airfoil aerodynamics: three different flow patterns within an angle of attack range of four degrees [C] . Bjoern F. Klose, Gustaaf B. Jacobs, Joseph Tank, AIAA fluid dynamics conference;AIAA aviation forum . 2018

机译：低雷诺数翼型空气动力学：攻角在4度范围内的三种不同流型
5. Modeling the rolling moment on the 65-degree delta wing for rolling motions at high angle of attack. [D] . Myatt, James Harold. 1997

机译：对65度三角翼上的侧倾力矩进行建模，以实现高攻角下的侧倾运动。
6. Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps [O] . Rinoie K. 1996

机译：带有涡流襟翼的60度圆形前缘三角翼的低速空气动力学特性
7. Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing [R] . Wiley, Harleth G 1952

机译：空气动力学特性扩展到小型0度扫掠翼，45度后掠翼和60度三角翼的跨音速时的大迎角

An experimental investigation of the effect of Reynolds number on the low speed aerodynamic characteristics of a delta wing space shuttle orbiter concept at angles of attack to 45 degrees

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