Experimental research and calculation of parameters of hypersonic separated flow around aerodynamic flaps under their interference

Kalugin V. T.; Chernukha P. A.

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Experimental research and calculation of parameters of hypersonic separated flow around aerodynamic flaps under their interference

机译：气动襟翼干扰下高超音速分离流参数的实验研究与计算。

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Various combinations of aft body flaps have been examined to determine the effectiveness of control of flow around cone-shaped bodies. Possible structures of flow around controls and their transformation depending on construction and gasdynamic parameters have been revealed. The applicable mathematical model is developed and parameteric calculations are conducted to determine aerodynamic characteristics of such bodies with flaps under the hypersonic flow conditions.

机译：已经检查了后身襟翼的各种组合，以确定控制锥形身周围流动的有效性。已经揭示了控件周围可能的流动结构及其取决于构造和气体动力学参数的转换。开发了适用的数学模型，并进行了参数计算，以确定在高超声速流动条件下带有襟翼的此类车身的空气动力学特性。

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《Вестник Московского государственного технического университета. Серия машиностроение》 |2001年第1期|共10页
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Kalugin V. T.; Chernukha P. A.;
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1. Experimental research and calculation of parameters of hypersonic separated flow around aerodynamic flaps under their interference [J] . Kalugin V. T., Chernukha P. A. Вестник Московского государственного технического университета. Серия машиностроение . 2001,第1期

机译：气动襟翼干扰下高超音速分离流参数的实验研究与计算。
2. Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap [J] . Thomas J. Horvath, Tod F. OConnell, F. McNeil Cheatwood, Journal of Spacecraft and Rockets . 2006,第2期

机译：带有襟翼的Mars Surveyor 2001精密着陆器的实验高超声速空气动力学特性
3. Study of the Aerodynamic Stability of a Blunt Cone with a Side Flap in a Hypersonic Flow [J] . A. V. Krasilnikov, G. G. Mordvintsev, V. N. Shmanenkov Fluid Dynamics . 2007,第1期

机译：超音速流中带有侧翼的钝锥的气动稳定性研究
4. Experimental Hypersonic Aerodynamic Characteristics of the Mars Surveyor 2001 Precision Lander with Flap [C] . T. Horvath, T. O, R. Prabhu, AIAA Guidance, Navigation, and Control Conference and Exhibit . 2002

机译：带有襟翼的Mars Surveyor 2001精密着陆器的实验高超声速空气动力学特性
5. Development of Advanced Techniques for Aerodynamic Assessment of Blunt Bodies in Hypersonic Flows [D] . Fisher, Thomas B. 2019

机译：高超声波钝体空气动力学评估的先进技术
6. Calculation and Identification of the Aerodynamic Parameters for Small-Scaled Fixed-Wing UAVs [O] . Jieliang Shen, Yan Su, Qing Liang, 2018

机译：小型固定翼无人机的空气动力学参数计算与识别
7. Experimental Hypersonic Aerodynamic Characteristics of the 2001 Mars Surveyor Precision Lander with Flap [O] . Prabhu Ramadas K., Horvath Thomas J., Cheatwood F. McNeil, 2002

机译：2001年火星测量员精密襟翼着陆器的高超声速空气动力学特性

Experimental research and calculation of parameters of hypersonic separated flow around aerodynamic flaps under their interference

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