首页> 美国政府科技报告 >COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLE

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COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLE

机译：在JpL 20-in曲线壁上计算的测量边界层厚度的比较。 sUpERsONIC WIND TUNNEL TWODImENsIONaL NOZZLE

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摘要

Boundary layer thickness on curved walls of 20-in supersonic wind tunnel two-dimensional nozzle

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作者
Dayman, B., Jr.;
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作者单位

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年度 1963
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BOUNDARY LAYERS; NOZZLE WALLS; REYNOLDS NUMBER; SUPERSONIC WIND TUNNELS; THICKNESS; TWO DIMENSIONAL BODIES; WALLS; WIND TUNNEL APPARATUS; BOUNDARY LAYER; NOZZLE WALL; SUPERSONIC WIND TUNNEL APPARATUS; TWO-DIMENSIONAL BODY;

机译：边界层;喷嘴墙; REYNOLDs NUmBER;超级风洞;厚度;二维机构;墙;风洞隧道设备;边界层;喷泉墙; sUpERsONIC WIND TUNNEL appaRaTUs;二维身体;

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1. Short communication/Comparison of measured and calculated thicknesses of martensite and ledeburite shells around graphite nodules in hardened layer after laser surface remelting [J] . J. Grum, R. Sturm Materials Science and Technology: MST: A publication of the Institute of Metals . 2002,第1期

机译：激光表面重熔后，硬化层中石墨球周围的马氏体和莱氏体壳的测量厚度和计算厚度的简短通信/比较
2. Comparison of measured and calculated thicknesses of martensite and ledeburite shells around graphite nodules in hardened layer after laser surface remelting [J] . J. Grum, R. Sturm Materials Science and Technology: MST: A publication of the Institute of Metals . 2002,第1期

机译：激光表面重熔后硬化层中石墨小球周围马氏体和莱氏体壳的测量和计算厚度的比较
3. Wind loads on rainscreen walls: Boundary-layer wind tunnel experiments [J] . Kala S, Stathopoulos T, Kumar KS Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2008,第6a7期

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4. Boundary-layer studies in a 2-D supersonic nozzle for quiet-tunnel applications [C] . Anthony Demetriades, Robert L. Mueller, Daniel C. Reda, 18th AIAA Aerospace Ground Testing Conference June 20-23, 1994/Colorado Springs, CO . -1

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5. Wind tunnel testing of a supersonic cruise nozzle in subsonic ejector configuration. [D] . Jones, Jesse Thomas. 2009

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6. Geometry Optimization of Supersonic Wind Tunnel Nozzle 2nd Report Verification of Optimization Method. [O] . Ryo NOMURA, Hideki KAWAMOTO, Takeshi YONEDA, 2003

机译：超音速风洞喷嘴的几何优化2nd报告优化方法验证。

COMPARISON OF CALCULATED WITH MEASURED BOUNDARY-LAYER THICKNESSES ON THE CURVED WALLS OF THE JPL 20-IN. SUPERSONIC WIND TUNNEL TWODIMENSIONAL NOZZLE

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