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 |
Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream
Title | Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream PDF eBook |
Author | Robert A. Wasko |
Publisher | |
Pages | 24 |
Release | 1962 |
Genre | Heat |
ISBN |
Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5
Title | Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5 PDF eBook |
Author | Thorval Tendeland |
Publisher | |
Pages | 28 |
Release | 1959 |
Genre | Aerodynamic heating |
ISBN |
The heat-transfer data obtained from the model were found to correlate when the T' method of Sommer and Short was used. The increase in turbulent heat-transfer rate with a reduction in wall to free-stream temperature ratio was of the same order of magnitude as has been found for the turbulent skin-friction coefficient.
Pressure and Heat-transfer Distributions of 0.1-scale Gemini Exit and Reentry Models at Mach Numbers of 3.51 and 4.44
Title | Pressure and Heat-transfer Distributions of 0.1-scale Gemini Exit and Reentry Models at Mach Numbers of 3.51 and 4.44 PDF eBook |
Author | |
Publisher | |
Pages | 116 |
Release | 1965 |
Genre | |
ISBN |
Heat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 from Flight Investigations of a Flat-face-cone and a Hemisphere-cone
Title | Heat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 from Flight Investigations of a Flat-face-cone and a Hemisphere-cone PDF eBook |
Author | Katherine C. Speegle |
Publisher | |
Pages | 60 |
Release | 1958 |
Genre | |
ISBN |
Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls
Title | Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations with Aerodynamic Controls PDF eBook |
Author | Louis G. Kaufman |
Publisher | |
Pages | 214 |
Release | 1964 |
Genre | Aircraft cabins |
ISBN |
Pressure data were obtained for Mach five flows over winged re-entry configurations composed of cylindrical cabins mounted on a 60 degree sweepback delta wing with a cylindrical leading edge, clipped tips, and trailing edge flaps. The model was tested with spherical and conical fronts on the cabin, with and without tip fins, and with and without a trailing edge spoiler. Flap deflections were varied from -40 to +40 degrees and the model was pitched at angles of attack from -30 to +45 degrees for a free stream Reynolds number, based on model length of 3,575,000. (Author)
Heat Transfer and Pressure Distributions at a Mach Number of 6 for 70 Swept Slab Wings with Sharp and Spherical Noses and Cylindrical Leading Edges
Title | Heat Transfer and Pressure Distributions at a Mach Number of 6 for 70 Swept Slab Wings with Sharp and Spherical Noses and Cylindrical Leading Edges PDF eBook |
Author | Robert A. Jones |
Publisher | |
Pages | 40 |
Release | 1962 |
Genre | |
ISBN |