Read Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone

Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone

Kuei-Yuan Chien

4.9/5 (34071 ratings)

Description:Turbulent skin-friction coefficients directly measured on an axisymmetric five-degree-half-angle sharp cone by two floating-element skin-friction balances at a free-stream Mach number of 7.9 are presented. Heat-transfer distributions are obtained simultaneously. These results yield directly the Reynolds analogy factor. Experimental data are used to evaluate four predictive methods. Except for the relatively low-Reynolds-number case, the directly measured sharp-cone Reynolds analogy factor is between 1.01 and 1.07, which is in good agreement with recent flat-plate measurements. Results indicate that the Stanton Number is essentially constant for one range and decreases by about 10 percent in another. (Modified author abstract).We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone. To get started finding Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone, you are right to find our website which has a comprehensive collection of manuals listed.
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Pages: 46

Format: PDF, EPUB & Kindle Edition

Publisher: —

Release: 1973

ISBN: 0x801vYgVIIC

Description: Turbulent skin-friction coefficients directly measured on an axisymmetric five-degree-half-angle sharp cone by two floating-element skin-friction balances at a free-stream Mach number of 7.9 are presented. Heat-transfer distributions are obtained simultaneously. These results yield directly the Reynolds analogy factor. Experimental data are used to evaluate four predictive methods. Except for the relatively low-Reynolds-number case, the directly measured sharp-cone Reynolds analogy factor is between 1.01 and 1.07, which is in good agreement with recent flat-plate measurements. Results indicate that the Stanton Number is essentially constant for one range and decreases by about 10 percent in another. (Modified author abstract).We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone. To get started finding Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.

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Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone

Hypersonic, Turbulent, Cold-wall, Skin-friction and Heat-transfer Measurements on an Axisymmetric Sharp Cone

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