Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15
Title | Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 Degree Half-cone Body (semidisk) at a Mach Number of 6.15 PDF eBook |
Author | P. Calvin Stainback |
Publisher | |
Pages | 21 |
Release | 1963 |
Genre | |
ISBN |
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Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15
Title | Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15 PDF eBook |
Author | P. Calvin Stainback |
Publisher | |
Pages | 20 |
Release | 1963 |
Genre | |
ISBN |
Download Pressure and Heat-transfer Maesurements on the Flat Face of a Blunted 10° Half-cone Body (semidisk) at a Mach Number of 6.15 Book in PDF, Epub and Kindle
Applied Mechanics Reviews
Title | Applied Mechanics Reviews PDF eBook |
Author | |
Publisher | |
Pages | 1196 |
Release | 1963 |
Genre | Mechanics, Applied |
ISBN |
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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°
Title | 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° PDF eBook |
Author | Raul Jorge Conti |
Publisher | |
Pages | 38 |
Release | 1961 |
Genre | Heat |
ISBN |
Download 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° Book in PDF, Epub and Kindle
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.
Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95
Title | Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 PDF eBook |
Author | Jerome D. Julius |
Publisher | |
Pages | 32 |
Release | 1959 |
Genre | Heat |
ISBN |
Download Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 Book in PDF, Epub and Kindle
Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10
Title | Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 PDF eBook |
Author | J. David Dearing |
Publisher | |
Pages | 28 |
Release | 1969 |
Genre | Aerodynamic heating |
ISBN |
Download Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 Book in PDF, Epub and Kindle
Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊
Title | Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ PDF eBook |
Author | Dennis M. Bushnell |
Publisher | |
Pages | 40 |
Release | 1968 |
Genre | Aerodynamics |
ISBN |
Download Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ Book in PDF, Epub and Kindle