Author: L. H. Back
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 925
Book Description
Heat-transfer Measurements in the Shock-induced Flow Separation Region in a Supersonic Nozzle
Author: L. H. Back
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 925
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 925
Book Description
Heat Transfer and Boundary Layer Measurements in a Region of Supersonic Flow Separation and Reattachment
Author: A. Naysmith
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 456
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 456
Book Description
Technical Report - Jet Propulsion Laboratory, California Institute of Technology
Author: Jet Propulsion Laboratory (U.S.)
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 28
Book Description
Heat Transfer 1970
Author: Ulrich Grigull
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 586
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 586
Book Description
Space Programs Summary
Author: Jet Propulsion Laboratory (U.S.)
Publisher:
ISBN:
Category : Space flight
Languages : en
Pages : 390
Book Description
Publisher:
ISBN:
Category : Space flight
Languages : en
Pages : 390
Book Description
Turbulent-flow Separation Criteria for Overexpanded Supersonic Nozzles
Author: E. Leon Morrisette
Publisher:
ISBN:
Category : Stratified flow
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Stratified flow
Languages : en
Pages : 44
Book Description
Heat Transfer in the Laminar Supersonic Separated Flow Behind an Axisymmetrical Backward Facing Step
Author: Josef Rom
Publisher:
ISBN:
Category :
Languages : en
Pages : 55
Book Description
Heat transfer rates are measured in the separated and reattaching flow regions behind an axisymmetrical backward facing step on a cone-cylinder model, in the high enthalpy laminar supersonic flow in the shock tube. The variation of the local heat transfer rate, divided by the equivalent attached heat transfer rate, behind the separation point is presented at various flow conditions. Shown, also, are the variations of the maximum and average heat transfer rates as functions of Reynolds and shock Mach numbers. Local heat transfer rates are found to vary with distance behind the step and to depend on the combination of Reynolds and shock Mach numbers. The heat transfer rate increases rapidly in the reattachment region and then decreases a little in the attached flow. Both the separation minimum heat transfer rate and the reattachment peak value increase when the Reynolds number is increased and Mach number decreased simultaneously. Peak values from 0.6 to 4 times the equivalent attached values are measured. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 55
Book Description
Heat transfer rates are measured in the separated and reattaching flow regions behind an axisymmetrical backward facing step on a cone-cylinder model, in the high enthalpy laminar supersonic flow in the shock tube. The variation of the local heat transfer rate, divided by the equivalent attached heat transfer rate, behind the separation point is presented at various flow conditions. Shown, also, are the variations of the maximum and average heat transfer rates as functions of Reynolds and shock Mach numbers. Local heat transfer rates are found to vary with distance behind the step and to depend on the combination of Reynolds and shock Mach numbers. The heat transfer rate increases rapidly in the reattachment region and then decreases a little in the attached flow. Both the separation minimum heat transfer rate and the reattachment peak value increase when the Reynolds number is increased and Mach number decreased simultaneously. Peak values from 0.6 to 4 times the equivalent attached values are measured. (Author).
Bibliography
Author: Jet Propulsion Laboratory (U.S.)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 92
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.