The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 PDF Download

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The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4

The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 PDF Author: Howard W. Stone
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Book Description

The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4

The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 PDF Author: Howard W. Stone
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Book Description

The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4

The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4 PDF Author: Howard W. Stone
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7

Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7 PDF Author: Marcus O. Creager
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36

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Book Description

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 PDF Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

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Book Description

The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7

The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7 PDF Author: Thorval Tendeland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

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Book Description

The Compressible Laminar Boundary Layer with Fluid Injection

The Compressible Laminar Boundary Layer with Fluid Injection PDF Author: George M. Low
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 38

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Book Description
A solution of the equations of the compressible laminar boundary layer including the effects of transpiration cooling is presented. The analysis applies to the flow over an isothermal porous plate with a velocity of fluid injection proportional to the reciprocal of the square root of the distance from the leading edge.

The Leading-edge Effects on a Laminar Flat-plane Boundary Layer at Mach 10.4

The Leading-edge Effects on a Laminar Flat-plane Boundary Layer at Mach 10.4 PDF Author: Howard W. Stone
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 206

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Book Description

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 PDF Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44

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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

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Book Description

Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate

Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate PDF Author: Don W. Jillie
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36

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Book Description