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The Calculation Of Compressible Turbulent Boundary Layers With Fluid Injection


The Calculation Of Compressible Turbulent Boundary Layers With Fluid Injection
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The Calculation Of Compressible Turbulent Boundary Layers With Fluid Injection


The Calculation Of Compressible Turbulent Boundary Layers With Fluid Injection
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Author : L. C. Squire
language : en
Publisher:
Release Date : 1973

The Calculation Of Compressible Turbulent Boundary Layers With Fluid Injection written by L. C. Squire and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Fluid dynamics categories.




The Compressible Turbulent Boundary Layer With Surface Mass Transfer


The Compressible Turbulent Boundary Layer With Surface Mass Transfer
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Author : Fred Culick
language : en
Publisher:
Release Date : 1960

The Compressible Turbulent Boundary Layer With Surface Mass Transfer written by Fred Culick and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Boundary layer categories.




Numerical Solution Of The Equations For Compressible Laminar Transitional And Turbulent Boundary Layers And Comparisons With Experimental Data


Numerical Solution Of The Equations For Compressible Laminar Transitional And Turbulent Boundary Layers And Comparisons With Experimental Data
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Author : Julius E. Harris
language : en
Publisher:
Release Date : 1971

Numerical Solution Of The Equations For Compressible Laminar Transitional And Turbulent Boundary Layers And Comparisons With Experimental Data written by Julius E. Harris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aerodynamics, Hypersonic categories.


A numerical method for solving the equations for laminar, transitional, and turbulent compressible boundary layers for either planar or axisymmetric flows is presented. The fully developed turbulent region is treated by replacing the Reynolds stress terms with an eddy viscosity model. The mean properties of the transitional boundary layer are calculated by multiplying the eddy viscosity by an intermittency function based on the statistical production and growth of the turbulent spots. A specifiable turbulent Prandtl number relates the turbulent flux of heat to the eddy viscosity. A three-point implicit finite-difference scheme is used to solve the system of equations. The momentum and energy equations are solved simultaneously without iteration. Numerous test cases are compared with experimental data for supersonic and hypersonic flows; these cases include flows with both favorable and mildly unfavorable pressure gradient histories, mass flux at the wall, and traverse curvature.



Approximate Formulas For The Computation Of Turbulent Boundary Layer Momentum Thicknesses In Compressible Flows


Approximate Formulas For The Computation Of Turbulent Boundary Layer Momentum Thicknesses In Compressible Flows
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Author : Neal Tetervin
language : en
Publisher:
Release Date : 1946

Approximate Formulas For The Computation Of Turbulent Boundary Layer Momentum Thicknesses In Compressible Flows written by Neal Tetervin and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Aerodynamics categories.


Summary: Approximate formulas for the computation of the momentum thicknesses of turbulent boundary layers on two-dimensional bodies, on bodies of revolution at zero angle of attack, and on the inner surfaces of round channels all in compressible flow are given in the form of integrals that can be conveniently computed. The formulas involve the assumptions that the momentum thickness may be computed by use of a boundary-layer velocity profile which is fixed and that skin-friction formulas for flat plates may be used in the computation of boundary-layer thicknesses in flow with pressure gradients. The effect of density changes on the ration of the displacement thickness to the momentum thickness of the boundary layer is taken into account. Use is made of the experimental finding that the skin-friction coefficient for turbulent flow is independent of Mach number. The computations indicated that the effect of density changes on the momentum thickness in flows with pressure gradients is small for subsonic flows.



Compressible Turbulent Boundary Layers With Combined Air Injection And Pressure Gradient


Compressible Turbulent Boundary Layers With Combined Air Injection And Pressure Gradient
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Author : G. D. Thomas
language : en
Publisher:
Release Date : 1976

Compressible Turbulent Boundary Layers With Combined Air Injection And Pressure Gradient written by G. D. Thomas and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Boundary layer categories.




Calculation Methods For Compressible Turbulent Boundary Layers 1976


Calculation Methods For Compressible Turbulent Boundary Layers 1976
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Author : Dennis M. Bushnell
language : en
Publisher:
Release Date : 1977

Calculation Methods For Compressible Turbulent Boundary Layers 1976 written by Dennis M. Bushnell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Compressibility categories.




Recent Advances In The Aerospace Sciences


Recent Advances In The Aerospace Sciences
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Author : Corrado Casci
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06

Recent Advances In The Aerospace Sciences written by Corrado Casci and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Science categories.


This volume, published in honor of Prof. Luigi Crocco, appears when Luigi Crocco celebrates his 75th birthday of a life devoted to study, research, and teaching. The events in his life and World War II forced Luigi Crocco, as well as other Italian scientists, to look to foreign countries for the calm haven so vital to study. This notwithstanding, his scientific activity was never inter rupted, and this volume is an acknowledgment of scientists and researchers to his work and life. Prefazione Questo volume in onore del prof. ing. Luigi Crocco vede la luce quando Luigi Crocco compie i 75 anni di una vita dedicata allo studio, alia ricerca e all'insegnamento. a Le vicende della vita, ed anche della 2 guerra mondiale, hanno costretto Luigi Crocco, come altri scienziati italiani, a dover cercare in altri Paesi quella serenita necessaria per dedicarsi allo studio. Ma la sua attivita scientifica non ha avuto interruzioni e questo volume essere la testimonianza di studiosi e di ricercatori alia sua opera e alia sua vita."



Analysis Of Turbulent Boundary Layers


Analysis Of Turbulent Boundary Layers
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Author : Tuncer Cebeci
language : en
Publisher: Elsevier
Release Date : 2012-12-02

Analysis Of Turbulent Boundary Layers written by Tuncer Cebeci and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-02 with Technology & Engineering categories.


Analysis of Turbulent Boundary Layers focuses on turbulent flows meeting the requirements for the boundary-layer or thin-shear-layer approximations. Its approach is devising relatively fundamental, and often subtle, empirical engineering correlations, which are then introduced into various forms of describing equations for final solution. After introducing the topic on turbulence, the book examines the conservation equations for compressible turbulent flows, boundary-layer equations, and general behavior of turbulent boundary layers. The latter chapters describe the CS method for calculating two-dimensional and axisymmetric laminar and turbulent boundary layers. This book will be useful to readers who have advanced knowledge in fluid mechanics, especially to engineers who study the important problems of design.



Calculation Methods For Compressible Turbulent Boundary Layers 1976


Calculation Methods For Compressible Turbulent Boundary Layers 1976
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Author : Dennis M. Bushnell
language : en
Publisher:
Release Date : 1977

Calculation Methods For Compressible Turbulent Boundary Layers 1976 written by Dennis M. Bushnell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Turbulent boundary layer categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date :

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.