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An evaluation of free-flight test data for aerodynamic heating from laminar, turbulent, and transitional boundary layers. Part II - The X-17 reentry body

机译：评估层流，湍流和过渡边界层空气动力加热的自由飞行试验数据。第二部分 - X-17再入体

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摘要

Blunt body reentry vehicle aerodynamic heating determination

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作者
Murphy, J. D.; Rubesin, M. W.;
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年度 1965
页码 1-93
总页数 93
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEATING; BLUNT BODIES; COMPARISON; REENTRY VEHICLES; TURBULENT BOUNDARY LAYER; WIND TUNNEL TESTS; X-17 REENTRY VEHICLE; AERODYNAMIC HEATING; BLUNT BODY; REENTRY VEHICLE;

机译：空气动力加热; BLUNT BODIEs;比较; REENTRY车辆;湍流边界层;风洞隧道测试; X-17 REENTRY车辆;空气动力加热; BLUNT BODY; REENTRY VEHICLE;

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专利

1. LAMINAR-TURBULENT TRANSITION IN BOUNDARY LAYERS (REVIEW). PART. 1: MAIN TYPES OF LAMINAR-TURBULENT TRANSITION IN A SWEPT-WING BOUNDARY LAYER [J] . M. V. Ustinov TsAGI science journal . 2013,第1期

机译：边界层中的层流湍流过渡（综述）。部分。 1：掠翼边界层中层流湍流的主要类型
2. SIMULATION ON LAMINAR-TO-TURBULENT TRANSITION OVER AN ABLATING REENTRY BODY [J] . KIMIYA KOMURASAKI, MASAKI KUWABARA, GRAHAM CANDLER 日本航空宇宙学会誌 . 1999,第540期

机译：消融折返体上层流向湍流转换的模拟
3. Computational study of a bluff body aerodynamics: Impact of the laminar-to-turbulent transition modelling [J] . International Journal of Mechanical Sciences . 2020,第期

机译：诈唬体空气动力学的计算研究：层流动湍流过渡建模的影响
4. Numerical investigation of laminar-turbulent transition in the boundary-layer of reentry capsules [C] . E.Laurien AIAA 33rd Aerospace Seicnces Meeting and Exhibit January 9-12, 1995/Reno, NV . 1995

机译：再入舱边界层内层流湍流过渡的数值研究
5. Experimental verification of a heat/mass transfer analogy in two dimensional laminar and turbulent boundary layers. [D] . Kulkarni, Kaustubh Shankar. 2008

机译：在二维层流和湍流边界层中进行热/质传递类比的实验验证。
6. Evaluation of a recombinant human T-cell lymphotropic virus type I (HTLV-I) p21E antibody detection enzyme immunoassay as a supplementary test in HTLV-I/II antibody testing algorithms. [O] . T M Hartley, G E Malone, R F Khabbaz, 1991

机译：对重组人I型T细胞淋巴病毒I（HTLV-1）p21E抗体检测酶免疫分析的评估作为HTLV-I / II抗体测试算法中的补充测试。
7. Laminar-Turbulent Transition of Three-Dimensional Boundary Layers. [O] . Ryoji Kobayashi 1994

机译：三维边界层的层压湍流转变。

An evaluation of free-flight test data for aerodynamic heating from laminar, turbulent, and transitional boundary layers. Part II - The X-17 reentry body

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