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Preliminary Investigation of the Transfer of Heat from a Flat Plate at a Mach Number of 1.5

Preliminary Investigation of the Transfer of Heat from a Flat Plate at a Mach Number of 1.5 PDF Author: Jr. M. A. Emmons
Publisher:
ISBN:
Category :
Languages : en
Pages : 23

Book Description

Preliminary Investigation of the Transfer of Heat from a Flat Plate at a Mach Number of 1.5

Preliminary Investigation of the Transfer of Heat from a Flat Plate at a Mach Number of 1.5 PDF Author: Jr. M. A. Emmons
Publisher:
ISBN:
Category :
Languages : en
Pages : 23

Book Description

Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106

Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106 PDF Author: James R. Hall
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34

Book Description

Preliminary Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61

Preliminary Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61 PDF Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Body of revolution
Languages : en
Pages : 30

Book Description

An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0

An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0 PDF Author: Paul F. Holloway
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 106

Book Description

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution PDF Author: Raul J. Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36

Book Description

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1132

Book Description

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description

An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free-stream Velocity

An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined with the Free-stream Velocity PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 34

Book Description

Research Abstracts

Research Abstracts PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568

Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 482

Book Description

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