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：干扰空气动力学襟翼周围超声波分离流程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：已经检查了各种组合的后体襟翼，以确定锥形体周围的流动控制的有效性。揭示了对控制的可能流动结构，根据施工和胃动力学参数进行转换。开发了适用的数学模型，并进行参数计算，以确定在超声波流动条件下用襟翼的这种体的空气动力学特征。

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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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