Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees

Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees
Title Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees PDF eBook
Author Dennis M. Bushnell
Publisher
Pages 38
Release 1968
Genre
ISBN

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Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊

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

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Heat-transfer and Pressure Distribution on Spherically Blunted 25° Half-angle Cone at Mach 8 and Angles of Attack Up to 90°

Heat-transfer and Pressure Distribution on Spherically Blunted 25° Half-angle Cone at Mach 8 and Angles of Attack Up to 90°
Title Heat-transfer and Pressure Distribution 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 38
Release 1968
Genre
ISBN

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NASA Technical Note

NASA Technical Note
Title NASA Technical Note PDF eBook
Author
Publisher
Pages 450
Release 1969
Genre
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°

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

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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.

NASA Technical Paper

NASA Technical Paper
Title NASA Technical Paper PDF eBook
Author
Publisher
Pages 92
Release 1983
Genre Science
ISBN

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Pressures, Forces, Moments and Shock Shapes for a Geometrically Matched Sphere-cone and Hyperboloid at Mach 20.3 in Helium

Pressures, Forces, Moments and Shock Shapes for a Geometrically Matched Sphere-cone and Hyperboloid at Mach 20.3 in Helium
Title Pressures, Forces, Moments and Shock Shapes for a Geometrically Matched Sphere-cone and Hyperboloid at Mach 20.3 in Helium PDF eBook
Author
Publisher
Pages 80
Release 1983
Genre
ISBN

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