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 Download

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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 PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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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 PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Book Description

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 ̊ PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

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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° PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 450

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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° PDF Author: Raul Jorge Conti
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 38

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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 PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 92

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A Selected Listing of NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478

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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 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 80

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Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50, ̊ 70, ̊ and 90

Heat Transfer to the Windward Side of a Fineness-ratio-2.9 Cylinder with Nearly Spherical Ends at a Mach Number of 6 and Angles of Attack of 50, ̊ 70, ̊ and 90 PDF Author: James Larry Hunt
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 50

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Book Description