Author: A. M. Kuethe
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Preliminary Results on the Turbulent Mixing of Supersonic Jets
Investigation with an Interferometer of the Turbulent Mixing of a Free Supersonic Jet
Author: Paul B. Gooderum
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
The free turbulent mixing of a supersonic jet was investigated with an interferometer, of which a description is given. Density and velocity distributions through the mixing zone were obtained. The velocity distribution was found to be similar to those for imcompressible jets over only the subsonic portion of the mixing pattern.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
The free turbulent mixing of a supersonic jet was investigated with an interferometer, of which a description is given. Density and velocity distributions through the mixing zone were obtained. The velocity distribution was found to be similar to those for imcompressible jets over only the subsonic portion of the mixing pattern.
Turbulent Mixing Noise from Supersonic Jets
Multiscale Turbulence Effects in Supersonic Jets Exhausting Into Still Air
Author: Khaled Sayed Abdol-Hamid
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
A Study of the Turbulent Mixing Region of a Supersonic Jet Mixing with a Low Speed Flow
Multiscale Turbulence Effects in Supersonic Jets Exhausting Into Still Air
Author: Khaled S. Abdol-Hamid
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Mixing of Supersonic Jets Including the Effects of Transvere Pressure Gradient Using Difference Methods
Author: Anatole P. Kurkov
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
The usual boundary-layer equations describing the steady-state mixing of parallel jets are supplemented by the momentum equation in the direction normal to the flow. This allows detailed computation of the flow field in the mixing region and simultaneous computation of the outer inviscid flow. An explicit and an implicit finite difference scheme have been developed and applied in several illustrative examples. The examples include mixing of planar and axisymmetric supersonic jets of different composition with both matched and unmatched static pressures. Numerical results were compared with available experimental data obtained for the unmatched pressure case.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
The usual boundary-layer equations describing the steady-state mixing of parallel jets are supplemented by the momentum equation in the direction normal to the flow. This allows detailed computation of the flow field in the mixing region and simultaneous computation of the outer inviscid flow. An explicit and an implicit finite difference scheme have been developed and applied in several illustrative examples. The examples include mixing of planar and axisymmetric supersonic jets of different composition with both matched and unmatched static pressures. Numerical results were compared with available experimental data obtained for the unmatched pressure case.
Turbulent mixing in supersonic jets
Author: Krishnamurthy Viswanathan
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
supersonic mixing of jets and turbulent boundary layers
Author: harry e bailey, arnold m kuotho
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Turbulent Mixing in Supersonic High-temperature Exhaust Jets
Author: Lei-Yong Jiang
Publisher: National Library of Canada = Bibliothèque nationale du Canada
ISBN: 9780612073128
Category : Aerodynamics, Supersonic
Languages : en
Pages : 328
Book Description
Publisher: National Library of Canada = Bibliothèque nationale du Canada
ISBN: 9780612073128
Category : Aerodynamics, Supersonic
Languages : en
Pages : 328
Book Description