Heat Transfer and Pressure Distribution on Cone-cylinder-flaire Configuration with Boundary-layer Separation
Title | Heat Transfer and Pressure Distribution on Cone-cylinder-flaire Configuration with Boundary-layer Separation PDF eBook |
Author | Harold Ferguson |
Publisher | |
Pages | |
Release | 1962 |
Genre | |
ISBN |
Heat Transfer and Pressure Distribution on Cone-cylinder-flare Configuration with Boundary-layer Separation
Title | Heat Transfer and Pressure Distribution on Cone-cylinder-flare Configuration with Boundary-layer Separation PDF eBook |
Author | Harold Ferguson |
Publisher | |
Pages | 44 |
Release | 1962 |
Genre | Fluid mechanics |
ISBN |
Heat Transfer and Pressure Distribution on Cone-cylinder-flare Configuration with Boundary-layer Separation
Title | Heat Transfer and Pressure Distribution on Cone-cylinder-flare Configuration with Boundary-layer Separation PDF eBook |
Author | Harold Ferguson |
Publisher | |
Pages | 39 |
Release | 1962 |
Genre | |
ISBN |
Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration
Title | Hypersonic-turbulent Boundary-layer Separation Over a Cone-cylinder-flare Configuration PDF eBook |
Author | Arnold Polak |
Publisher | |
Pages | 56 |
Release | 1969 |
Genre | Aerodynamics, Hypersonic |
ISBN |
Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data were obtained for a cone-cylinder-flare configuration. The experimental data were correlated with a theoretical prediction. (Author).
NASA Technical Note
Title | NASA Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 402 |
Release | 1968 |
Genre | |
ISBN |
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 |
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.
Monthly Catalog of United States Government Publications
Title | Monthly Catalog of United States Government Publications PDF eBook |
Author | |
Publisher | |
Pages | 1990 |
Release | 1962 |
Genre | Government publications |
ISBN |