Flap effectiveness appraisal for winged re-entry vehicles

de Rosa Donato; Pezzella Giuseppe; Donelli Raffaele S.; Viviani Antonio

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Flap effectiveness appraisal for winged re-entry vehicles

机译：有翼再入车辆的襟翼有效性评估

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The interactions between shock waves and boundary layer are commonplace in hypersonic aerodynamics. They represent a very challenging design issue for hypersonic vehicle. A typical example of shock wave boundary layer interaction is the flowfield past aerodynamic surfaces during control. As a consequence, such flow interaction phenomena influence both vehicle aerodynamics and aerothermodynamics. In this framework, the present research effort describes the numerical activity performed to simulate the flow field past a deflected flap in hypersonic flowfield conditions for a winged re-entry vehicle. (C) 2016 IAA. Published by Elsevier Ltd. All rights reserved.

机译：冲击波和边界层之间的相互作用在高超音速空气动力学中是司空见惯的。对于超音速飞行器，它们代表了一个非常具有挑战性的设计问题。冲击波边界层相互作用的典型示例是在控制过程中经过空气动力学表面的流场。结果，这种流动相互作用现象影响了车辆的空气动力学和空气热力学。在这种框架下，本研究工作描述了数值活动，该活动用于模拟有翼再入飞行器在高超音速流场条件下经过偏转襟翼的流场。（C）2016 IAA。由Elsevier Ltd.出版。保留所有权利。

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来源
《Acta astronautica》 |2016年第mayajuna期|175-184|共10页
作者
de Rosa Donato; Pezzella Giuseppe; Donelli Raffaele S.; Viviani Antonio;
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作者单位

CIRA, I-81043 Capua, Italy;

CIRA, I-81043 Capua, Italy;

CIRA, I-81043 Capua, Italy;

Univ Naples 2, I-81031 Aversa, Italy;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Computational fluid dynamics; Hypersonic flow; Shock-wave-boundary layer interaction; Shock-shock interaction; Reacting flow;

机译：计算流体力学;人流;冲击波边界层相互作用;冲击-冲击相互作用;反应流;

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机译：机翼柔韧性对具有双翼拍打和飞行作用的悬停扑翼微型飞机产生力的实验研究
3. Modal analysis of an artificial wing mimicking an Allomyrina dichotoma beetle's hind wing for flapping-wing micro air vehicles by noncontact measurement techniques [J] . Ngoc San Ha, Tailie Tin, Nam Seo Goo Optics and Lasers in Engineering . 2013,第5期

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4. HYPERSONIC AERODYNAMIC APPRAISAL OF WINGED BLUNT, RATHER SHARP AND SPATULED BODY RE-ENTRY VEHICLES [C] . Antonio Viviani, Giuseppe Pezzella Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：翼形短发，棘轮锋利和花式车身重入车辆的超音速气动评估
5. The effects of wing flexibility on the flight performance and stability of flapping wing micro air vehicles. [D] . Bluman, James Edward. 2017

机译：机翼柔性对襟翼微型航空器飞行性能和稳定性的影响。
6. Batch fabrication process of biomimetic wing with high flexibility of stiffness design for flapping-wing micro aerial vehicles [O] . Takashi Ozaki, Kanae Hamaguchi 2020

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7. Experimental investigation of wing flexibility on force generation of a hovering flapping wing micro air vehicle with double wing clap-and-fling effects [O] . Quoc V Nguyen, Woei L Chan, Marco Debiasi 2017

机译：双翼拍摄杂交效应悬停翼微型空气车辆翼韧性翼柔性的实验研究
8. INVESTIGATION OF EFFECTIVENESS OF A WING EQUIPPED WITH A 50-PERCENT-CHORD SLIDING FLAP, A 30-PERCENTVCHORD SLOTTED FLAP, AND A 30-PERCENT-CHORD SLAT TN DEFLECTING PROPELLER SLIPSTREAMS DOWNWARD FOR VERTICAL TAKE-OFF [R] . Richard E. Kuhn 1957

机译：一个装有50％滑动翼片的翼的效果的调查，一个30％的槽开槽，以及一个30％的TaT sLaT TN向下旋转的螺旋桨sLIpsTREams向下垂直起飞

Flap effectiveness appraisal for winged re-entry vehicles

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