Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Laminar Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Book Description
Laminar Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 34
Book Description
Laminar Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack [with List of References]
Author:
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 15
Book Description
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 15
Book Description
Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 32
Book Description
Laminar Boundary-layer Separation Induced by Flares on Cylinders with Highly Cooled Boundary Layers at a Mach Number of 15
Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 38
Book Description
NASA Technical Report
Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack
Author: Donald M. Kuehn
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 36
Book Description
Separation caused by the pressure rise induced by flares has been experimentally investigated in the Mach number range of 1.5 to 5.0 and in the Reynolds number range (based on boundary-layer thickness) of 1.5X104 to 12X104. The purpose of the investigation was to determine the model geometry and flow conditions for which separation can be expected for a turbulent boundary layer of zero pressure gradient on the cylinder approaching the flare. Comparisons are made of the boundary-layer-separation characteristics of these three-dimensional flares with two-dimensional separation results from a previous investigation.
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 36
Book Description
Separation caused by the pressure rise induced by flares has been experimentally investigated in the Mach number range of 1.5 to 5.0 and in the Reynolds number range (based on boundary-layer thickness) of 1.5X104 to 12X104. The purpose of the investigation was to determine the model geometry and flow conditions for which separation can be expected for a turbulent boundary layer of zero pressure gradient on the cylinder approaching the flare. Comparisons are made of the boundary-layer-separation characteristics of these three-dimensional flares with two-dimensional separation results from a previous investigation.