Author: Howard W. Stone
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4
Author: Howard W. Stone
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4
Author: Howard W. Stone
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7
Author: Marcus O. Creager
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44
Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46
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
Author: Thorval Tendeland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
Book Description
The Compressible Laminar Boundary Layer with Fluid Injection
Author: George M. Low
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 38
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.
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 38
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
Author: Howard W. Stone
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 206
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 206
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
Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44
Book Description
An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0
Author: Paul F. Holloway
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 106
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 106
Book Description
Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate
Author: Don W. Jillie
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
Book Description