Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10) PDF Download
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Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 46
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Book Description
Heat transfer data are presented for a Mach number range of 1.02 to 2.48 and for a Reynolds number range of 3,180,000 to 163,850,000 based on the axial distance from the nose to the point at which temperature measurements were made.
Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 46
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Book Description
Heat transfer data are presented for a Mach number range of 1.02 to 2.48 and for a Reynolds number range of 3,180,000 to 163,850,000 based on the axial distance from the nose to the point at which temperature measurements were made.
Author: Leo T Chauvin
Publisher:
ISBN:
Category :
Languages : en
Pages : 38
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Book Description
Author: Leo T. Chauvin
Publisher:
ISBN:
Category : Body of revolution
Languages : en
Pages : 38
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Book Description
Local coefficients of convective heat transfer have been evaluated from skin temperatures along the body of an NACA research missile designated RM-10. The general shape of the body was a parabola of revolution of fineness ratio 12.2. Heat-transfer data are presented for a Mach number range of 1.02 to 2.48 and for a Reynolds number range of 3,180,000 to 163,850,000 based on the axial distance from the nose to the point at which temperature measurements were made.
Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
ISBN: 9781013778704
Category :
Languages : en
Pages : 46
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Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1136
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 424
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Author: Max C. Kurbjun
Publisher:
ISBN:
Category : Noise
Languages : en
Pages : 742
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Book Description
Overall sound-pressure levels and frequency spectra of the noise emitted from a full-scale, 7.2-foot-diameter, 3, 500 rpm, three-blade, supersonic propeller mounted on a turbine-powered airplane have been obtained under static conditions at stations about the propeller at a 100-foot radius.
Author: Donald E. Coletti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
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Book Description
