Charts of Equilibrium Real-gas Stagnation Point Conditions on a Sphere for Altitudes to 200,000 Feet and Velocities to 15,000 Feet Per Second PDF Download
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Author: P. D. Fisher
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 60
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Book Description
This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).
Author: P. D. Fisher
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 60
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Book Description
This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).
Author: P. D. Fisher
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 998
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Book Description
Author: Richard L. Humphrey
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 60
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Book Description
Tests were made with a cylindrical model transpiration cooled over a region plus or minus 15 deg. from the stagnation line. Air was used as the coolant. The model was tested at a nominal Mach number of 7.0. Wall temperatures and heat-transfer rates were in good agreement with predicted values. The effect of the external pressure distribution on the local coolant flow rate and wall temperature is discussed. (Author).
Author: Harvard Lomax
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 96
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 666
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 510
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Book Description
Author:
Publisher:
ISBN:
Category : American literature
Languages : en
Pages : 654
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Book Description
Author:
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 658
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Book Description
Author:
Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 656
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Book Description
Includes entries for maps and atlases.
