Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Axial Forces on Cone-Cylinders in Transitional Rarefied Hypersonic Flow
Axial Forces on Cone-cylinders in Transitional Rarefied Hypersonic Flow
Author: David E. Boylan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 41
Book Description
Axial forces were measured on cone-cylinder configurations under hypersonic, cold wall, rarefied flow conditions. Measurements were obtained in the angle-of-attack range 0
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 41
Book Description
Axial forces were measured on cone-cylinder configurations under hypersonic, cold wall, rarefied flow conditions. Measurements were obtained in the angle-of-attack range 0
The Drag of Slender Axisymmetric Cones in Rarefied Hypersonic Flow
Author: T. J. Rhys-Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
This Paper describes an experimental study performed in the RAE Low Density Tunnel to determine the aerodynamic characteristics of a range of slender axisymmetric bodies in rarefied hypersonic flow. The main purpose of this study was to assess the effects of cone angle, nose bluntness and Reynolds number on the zero incidence drag of cones. In addition, some measurements of axial force, normal force and pitching moment at incidence were made. The bodies were tested at a nominal Mach number of 10 and at flow conditions which correspond to those in the transitional rarefied flow regime. These data have been compared with correlations developed to represent the change in drag coefficient in this flow regime between continuum and free molecular flow.
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
This Paper describes an experimental study performed in the RAE Low Density Tunnel to determine the aerodynamic characteristics of a range of slender axisymmetric bodies in rarefied hypersonic flow. The main purpose of this study was to assess the effects of cone angle, nose bluntness and Reynolds number on the zero incidence drag of cones. In addition, some measurements of axial force, normal force and pitching moment at incidence were made. The bodies were tested at a nominal Mach number of 10 and at flow conditions which correspond to those in the transitional rarefied flow regime. These data have been compared with correlations developed to represent the change in drag coefficient in this flow regime between continuum and free molecular flow.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1134
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1134
Book Description
Hypersonic Viscous Drag on Cones in Rarefied Flow
Author: Marvin I. Kussoy
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Measured Axial and Normal Force Coefficients for 9 C̊ones in Rarefied, Hypersonic Flow
Author: Desikan Bharathan
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 86
Book Description
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 86
Book Description
Lift and Drag on Cone Cylinders
Author: Theodore Conrad Nark
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 98
Book Description
Measurements of axial forces on cones in very rarefied, arc-heated nigrogen flows
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
Book Description
Induced Pressures and Shock Shapes on Blunt Cones in Hypersonic Flow
Author: Richard D. Wagner (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 40
Book Description
Cone Drag in Rarefied Hypersonic Flow
Author: Marvin I. Kussoy
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 6
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 6
Book Description