Author: Randall C. Maydew
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 60
Book Description
Velocity profiles at five axial stations in the half-jet mixing region of Mach 0.7, 0.85, 0.95, 1.49, and 1.96 free jets were measured. The nondimensional velocity distributions are similar, and correlate with the theory of Crane for incompressible flow. The half-jet spreading rate is essentially constsnt at subsonic speeds and decreases at supersonic speeds. The variation of jet spreading parameter with Mach number was determined from correlation of these and other data.
Turbulent Mixing of Axisymmetric Compressible Jets
Author: Randall C. Maydew
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 60
Book Description
Velocity profiles at five axial stations in the half-jet mixing region of Mach 0.7, 0.85, 0.95, 1.49, and 1.96 free jets were measured. The nondimensional velocity distributions are similar, and correlate with the theory of Crane for incompressible flow. The half-jet spreading rate is essentially constsnt at subsonic speeds and decreases at supersonic speeds. The variation of jet spreading parameter with Mach number was determined from correlation of these and other data.
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 60
Book Description
Velocity profiles at five axial stations in the half-jet mixing region of Mach 0.7, 0.85, 0.95, 1.49, and 1.96 free jets were measured. The nondimensional velocity distributions are similar, and correlate with the theory of Crane for incompressible flow. The half-jet spreading rate is essentially constsnt at subsonic speeds and decreases at supersonic speeds. The variation of jet spreading parameter with Mach number was determined from correlation of these and other data.
Turbulent Mixing of Axisymmetric Compressible Jets
Author: Randall C. Maydew
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 58
Book Description
Velocity profiles at five axial stations in the half-jet mixing region of Mach 0.7, 0.85, 0.95, 1.49, and 1.96 free jets were measured. The nondimensional velocity distributions are similar, and correlate with the theory of Crane for incompressible flow. The half-jet spreading rate is essentially constsnt at subsonic speeds and decreases at supersonic speeds. The variation of jet spreading parameter with Mach number was determined from correlation of these and other data.
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 58
Book Description
Velocity profiles at five axial stations in the half-jet mixing region of Mach 0.7, 0.85, 0.95, 1.49, and 1.96 free jets were measured. The nondimensional velocity distributions are similar, and correlate with the theory of Crane for incompressible flow. The half-jet spreading rate is essentially constsnt at subsonic speeds and decreases at supersonic speeds. The variation of jet spreading parameter with Mach number was determined from correlation of these and other data.
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 722
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 722
Book Description
Free Turbulent Mixing
Author: Philip Thomas Harsha
Publisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 340
Book Description
Publisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 340
Book Description
Proceedings
Author:
Publisher:
ISBN:
Category : Fluid amplifiers
Languages : en
Pages : 408
Book Description
Publisher:
ISBN:
Category : Fluid amplifiers
Languages : en
Pages : 408
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 724
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 724
Book Description
Compressibility Effects on Fluid Entrainment by Turbulent Mixing Layers
Author: Jacques Anselm Frederic Hill
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 1204
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 1204
Book Description
A Numerical Solution for the Interaction of a Moving Shock Wave with a Turbulent Mixing Region
Author: William Fred Walker
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 216
Book Description
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 216
Book Description
Proceedings of the Fluid Amplification Symposium
Author:
Publisher:
ISBN:
Category : Fluid amplifiers
Languages : en
Pages : 912
Book Description
Publisher:
ISBN:
Category : Fluid amplifiers
Languages : en
Pages : 912
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description