Aerodynamic Performances of Hypersonic Aircrafts with Surface Mass Transfer

N. I. Sidnyaev

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Aerodynamic Performances of Hypersonic Aircrafts with Surface Mass Transfer

机译：具有表面质量传递的高超音速飞机的空气动力学性能

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The results of investigations related to aerodynamic performances of a high-speed aircraft model, the body of which is designed in the form of rotary solids consisting of different combinations of conical bodies, for example, with permeable conical blunt-nosed body, if there is an active thermal protection, central cylindrical or poorly conical segment and with conical tailplane have been presented in the work. The profiles of pressure distribution over the body's surface under different angles of attack have been obtained. These profiles make it possible to obtain information about the dynamic perfor-mance of the aircraft and reactive drag.

机译：有关高速飞机模型的空气动力学性能的调查结果，该飞机的主体以旋转固体的形式设计，由各种不同的圆锥形体组合构成，例如，如果有的话，还带有可渗透的圆锥形钝头形体在工作中已经提出了一种主动的热保护，中心圆柱或圆锥差的部分以及圆锥形的尾板。已经获得了在不同迎角下人体表面上压力分布的分布图。这些配置文件可以获取有关飞机动态性能和反作用阻力的信息。

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来源
《Mathematical models and computer simulations》 |2009年第3期|共10页
作者
N. I. Sidnyaev;
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原文格式 PDF
正文语种 eng
中图分类数学;
关键词
Performances; Aircrafts; Mass Transfer;

机译：表演;飞机;大众转移;

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专利

1. Aerodynamic Performances of Hypersonic Aircrafts with Surface Mass Transfer [J] . N. I. Sidnyaev Mathematical models and computer simulations . 2009,第3期

机译：具有表面质量传递的高超音速飞机的空气动力学性能
2. Numerical Study of the Effect of Rotation on the Behavior of the Conjugate Heat and Mass Transfer on the Surface of a Spherically Blunted Cone Exposed to a Hypersonic Flow at an Angle of Attack with Ablation from the Surface [J] . Efimov K. N., Ovchinnikov V. A., Yakimov A. S. High temperature: English translation of teplofizika vysokikh temperatur . 2018,第2期

机译：旋转效果对张开锥体表面的缀合物热量和质量传递的作用，其暴露于表面的攻击角度钝化的过度流动
3. Aerodynamic configuration integration design of hypersonic cruise aircraft with inward-turning inlets [J] . Jifei WANG, Jinsheng CAI, Chuanzhen LIU, 中国航空学报（英文版） . 2017,第004期

机译：内向进气道的高超音速巡航飞机的气动配置一体化设计
4. The one-dimensional and two-dimensional inverse problems of heat and mass transfer on hypersonic aircraft permeable surfaces [C] . Grigory Bilchenko, Natalya Bilchenko 2017 Constructive Nonsmooth Analysis and Related Topics (dedicated to the memory of V.F. Demyanov) . 2017

机译：高超音速飞机可渗透表面传热和传质的一维和二维逆问题
5. Experimental and computational aerodynamic analysis of ice fragments shed from aircraft surfaces. [D] . Jacob, Joel. 2005

机译：从飞机表面喷出的冰块的实验和计算空气动力学分析。
6. Simulation Analysis of the Aerodynamic Performance of a Bionic Aircraft with Foldable Beetle Wings in Gliding Flight [O] . Caidong Wang, Yu Ning, Xinjie Wang, 2020

机译：仿生飞机在滑翔飞行中的仿生飞机空气性能的仿真分析
7. Modeling of coupled aerogasdynamics and heat transfer processes on the thermal protection surface of a future hypersonic aircraft [O] . Ю.И. Димитриенко, А.А. Захаров, М.Н. Коряков, 2014

机译：耦合气体动力学和传热过程的建模在未来超声波飞机的热保护表面
8. Pressure and Heat Transfer Measurements for Mach 8 Flows over a Blunt Pyramidal Configuration with Aerodynamic Controls. Part II: Pressure Data for Dihedral Surfaces (Part of an Investigation for Hypersonic Flow Separation and Control Characteristics) [R] . Kaufman, L. G. 1964

机译：采用空气动力学控制的钝化金字塔形结构的马赫数8流量的压力和传热测量。第二部分：二面体表面的压力数据（高超声速流动分离和控制特性研究的一部分）

Aerodynamic Performances of Hypersonic Aircrafts with Surface Mass Transfer

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