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Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90°

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Release : 1961
Genre : Heat
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Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul Jorge Conti

Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on a Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul Jorge Conti. This book was released on 1961. Available in PDF, EPUB and Kindle. Book excerpt: Two circulation conical configurations having 15° half-angles were tested in laminar boundary layer at a Mach number of 6 and angles of attack up to 90°. One cone had a sharp nose and a fineness ratio of 1.87 and the other had a spherically blunted nose with a bluntness ratio of 0.1428 and a fineness ratio of 1.66. Pressure measurements and schlieren pictures of the flow showed that near-conical flow existed above 70° high pressure areas were present near the base and the bow shock wave was considerably curved.

Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees

Download Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees PDF Online Free

Author :
Release : 1961
Genre :
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees by : RAUL J. CONTI

Download or read book Laminar Heat-transfer and Pressure Measurements at a Mach Number of 6 on Sharp and Blunt 15 Degree Half-angle Cones at Angles of Attack Up to 90 Degrees written by RAUL J. CONTI. This book was released on 1961. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer and pressure distributions were measured on sharp and blunt 15 degree half-angle cones. The flow was near conical on the windward side of the models up to an angle of attack of about 60 degrees. At angles of attack above 70 degrees the flow departed noticeably from conical characteristics. Heat-transfer and pressure measurements were found to agree satisfactorily with theories of simple application. At large angles of attack the effects of nose bluntness are very small in the region beyond two nose radii from the point of tangency. (Author).

Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90°

Download Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° PDF Online Free

Author :
Release : 1961
Genre :
Kind : eBook
Book Rating : /5 ( reviews)

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Book Synopsis Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° by : Raul J. Conti

Download or read book Laminar Heat-transfer and Pressure Measurement at a Mach Number of 6 on Sharp and Blunt 15° Half-angle Cones at Angles of Attack Up to 90° written by Raul J. Conti. This book was released on 1961. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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Author :
Release : 1962
Genre : Technology
Kind : eBook
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Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.). This book was released on 1962. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Government Research Reports

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Author :
Release : 1962
Genre : Science
Kind : eBook
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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by . This book was released on 1962. Available in PDF, EPUB and Kindle. Book excerpt:

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