An Investigation of the Effects of Heat Transfer on Boundary-layer Transition of a Parabilic Body of Revolution (NACA RM-10) at a Mach Number of 1.61 PDF Download

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

An Investigation of the Effects of Heat Transfer on Boundary-layer Transition of a Parabilic Body of Revolution (NACA RM-10) at a Mach Number of 1.61 PDF Author: K.R. Czarnecki
Publisher:
ISBN:
Category :
Languages : en
Pages : 11

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

An Investigation of the Effects of Heat Transfer on Boundary-layer Transition of a Parabilic Body of Revolution (NACA RM-10) at a Mach Number of 1.61 PDF Author: K.R. Czarnecki
Publisher:
ISBN:
Category :
Languages : en
Pages : 11

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AN EXTENSION 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

AN EXTENSION 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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 25

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 608

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Journal of the Royal Aeronautical Society

Journal of the Royal Aeronautical Society PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 976

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Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: D. Adamson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 366

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Handbook of Supersonic Aerodynamics

Handbook of Supersonic Aerodynamics PDF Author: Johns Hopkins University. Applied Physics Laboratory
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 372

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Investigation of the Variation with Reynolds Number of the Base, Wave, and Skin-friction Drag of a Parabolic Body of Revolution (NACA RM-10) at Mach Numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch Supersonic Tunnel

Investigation of the Variation with Reynolds Number of the Base, Wave, and Skin-friction Drag of a Parabolic Body of Revolution (NACA RM-10) at Mach Numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch Supersonic Tunnel PDF Author: Eugene S. Love
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 70

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A Pressure-distribution Investigation of a Fineness-ratio-12.2 Parabolic Body of Revolution (NACA RM-10) at M

A Pressure-distribution Investigation of a Fineness-ratio-12.2 Parabolic Body of Revolution (NACA RM-10) at M PDF Author: Morton Cooper
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 94

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Drag and Heat Transfer on a Parabolic Body of Revolution (N.A.C.A. RM-10) in Free Flight to Mach Number 2 with Both Constant and Varying Reynolds Number and Heating Effects on Turbulent Skin Friction

Drag and Heat Transfer on a Parabolic Body of Revolution (N.A.C.A. RM-10) in Free Flight to Mach Number 2 with Both Constant and Varying Reynolds Number and Heating Effects on Turbulent Skin Friction PDF Author: Joseph P. Maloney
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ISBN:
Category :
Languages : en
Pages : 34

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Skin-friction Drag and Boundary-layer Transition on a Parabolic Body of Revolution (N.A.C.A. RM-10) at a Mach Number of 1.6 in the Langley 4- by 4-foot Supersonic Pressure Tunnel

Skin-friction Drag and Boundary-layer Transition on a Parabolic Body of Revolution (N.A.C.A. RM-10) at a Mach Number of 1.6 in the Langley 4- by 4-foot Supersonic Pressure Tunnel PDF Author: K. R. Czarnecki
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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