Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody PDF Download

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Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody

Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody PDF Author: Mamoru Inouye
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description


Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody

Wind-tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone-cylinder with Flared Afterbody PDF Author: Mamoru Inouye
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description


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A Description of Numerical Methods and Computer Programs for Two-dimensional and Axisymmetric Supersonic Flow Over Blunt-nosed and Flared Bodies

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Category : Aerodynamics, Supersonic
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Wind-tunnel Measurements and Comparison with Flight of the Boundary Layer and Heat Transfer on a Hollow Cylinder at Mach 3

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