On Maximum Ballistic Coefficient Axisymmetric Geometries in Hypersonic Flows

Brahmachary Shuvayan; Natarajan Ganesh; Sahoo Niranjan

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On Maximum Ballistic Coefficient Axisymmetric Geometries in Hypersonic Flows

机译：高超音速流中的最大弹道系数轴对称几何

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来源
《Journal of Spacecraft and Rockets》 |2018年第2期|518-522|共5页
作者
Brahmachary Shuvayan; Natarajan Ganesh; Sahoo Niranjan;
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作者单位

Indian Inst Technol Guwahati, Dept Mech Engn, Gauhati 781039, Assam, India;

Indian Inst Technol Guwahati, Dept Mech Engn, Gauhati 781039, Assam, India;

Indian Inst Technol Guwahati, Dept Mech Engn, Gauhati 781039, Assam, India;

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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
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1. On the Use of High-Order Accurate Solutions of PNS Schemes as Basic Flows for Stability Analysis of Hypersonic Axisymmetric Flows [J] . Kazem Hejranfar, Vahid Esfahanian, Hossein Mahmoodi Darian Journal of Fluids Engineering: Transactions of the ASME . 2007,第10期

机译：关于使用PNS格式的高阶精确解作为基本流进行高超声速轴对称流稳定性分析
2. A Spectrally Accurate Two-Dimensional Axisymmetric,Tightly Coupled Photon Monte Carlo Radiative Transfer Equation Solver for Hypersonic Entry Flows [J] . A. M. Feldick, M. F. Modest Journal of Heat Transfer . 2012,第12期

机译：高超音速进入流的光谱精确二维轴对称紧耦合光子蒙特卡罗辐射传递方程求解器
3. Dual-code solution procedure for efficient computing equilibrium hypersonic axisymmetric transitional/turbulent flows [J] . Kazem Hejranfar, Vahid Esfahanian, Ramin Kamali-Moghadam Aerospace science and technology . 2012,第1期

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4. Influence of State-to-State Transport Coefficients on Surface Heat Transfer in Hypersonic Flows [C] . Eswar Josyula, Jonathan M. Burt, Elena Kustova, AIAA SciTech forum;Aerospace sciences meeting . 2014

机译：状态间的传输系数对高超声速流动中表面传热的影响
5. Experimental study on the effects of nose geometry on drag over axisymmetric bodies in supersonic flow. [D] . Brooker, B. Tyler. 2014

机译：鼻子几何形状对超声速流中轴对称物体上阻力的影响的实验研究。
6. Geometry Effects of Axisymmetric Flow-Focusing Microchannels for Single Cell Encapsulation [O] . Mohammad Nooranidoost, Ranganathan Kumar 2019

机译：轴对称流聚焦微通道的单细胞封装的几何效应。
7. An Experimental Study on Hypersonic Flow Using a Ballistic Range. (1). Photographic Measurement and Its Processing. [O] . Xin-yu CHANG, Makoto HEMMI, Akihiro SASOH, 1993

机译：弹道范围对超声波流动的实验研究。（1）。摄影测量及其加工。
8. COMPUTER CODE HRS015: A QUIKTRAN COMPUTER CODE FOR THE COMPUTATION OF THE TRANSITION FLOW HYPERSONIC BALLISTIC COEFFICIENT OF A BLUNT OBJECT, [R] . spahr, h. r. 1969

机译：计算机代码HRs015：一个QUIKTRaN计算机代码，用于计算一个对象的过渡流超音速弹道系数，

On Maximum Ballistic Coefficient Axisymmetric Geometries in Hypersonic Flows

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