Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer

DOWNLOAD

Download Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page

Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer

DOWNLOAD
Author : Robert L. P. Voisinet
language : en
Publisher:
Release Date : 1973

Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer written by Robert L. P. Voisinet 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 mechanics categories.

The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract).

Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer

DOWNLOAD
Author : Robert L. P. Voisinet
language : en
Publisher:
Release Date : 1973

Measurements Of A Supersonic Favorable Pressure Gradient Turbulent Boundary Layer With Heat Transfer written by Robert L. P. Voisinet 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 mechanics categories.

The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract).

Compressible Turbulent Skin Friction On Rough And Rough Wavy Walls In Adiabatic Flow

DOWNLOAD
Author : Daniel C. Reda
language : en
Publisher:
Release Date : 1974

Compressible Turbulent Skin Friction On Rough And Rough Wavy Walls In Adiabatic Flow written by Daniel C. Reda and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Fluid mechanics categories.

An experimental program was conducted to investigate effects of roughness, and roughness superimposed on single and/or multiple, shallow, periodic waveforms, on turbulent boundary-layer skin friction and velocity profile, in compressible, adiabatic flow. Test conditions were Mach number = 2.9 and Reynolds number/ft = 2 million to 8 million. The planar models included smooth, sand-grain, machined and molded surface finishes. Direct measurements of surface shear and Pitot/recovery temperature profiles were obtained. (Modified author abstract).

Scientific And Technical Aerospace Reports

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1995

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 1995 with Aeronautics categories.

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Temperature Step Effects On Direct Measurement Of Skin Friction Drag

DOWNLOAD
Author : Robert L. P. Voisinet
language : en
Publisher:
Release Date : 1977

Temperature Step Effects On Direct Measurement Of Skin Friction Drag written by Robert L. P. Voisinet and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Boundary layer categories.

Wall-temperature discontinuities can occur in skin-friction balance tests whenever a balance drag element is thermally insulated from the surrounding test surface. An experimental study was conducted to investigate the effects of such a temperature step on the local friction drag. A temperature step was produced by varying the temperature of the NSWC skin-friction-balance drag element above the temperature of the surrounding nozzle wall. Drag-element temperatures ranged from 100 K to 240 K with the surrounding wall maintained at a temperature of 89 K. Nominal Mach numbers were 2.9 and 4.9 over a unit Reynolds number range of 2.6 to 20 million per meter. The results show that the value of the measured shear stress is higher than the cold wall value for a drag element which is at a higher temperature than the surrounding wall temperature and the change in shear stress is proportional to the difference between the drag element and the surrounding wall temperatures. The data has been correlated and corrections to previously published skin-friction results are presented.

Government Reports Announcements

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1974

Government Reports Announcements written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Research categories.

Applied Mechanics Reviews

DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1974

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Mechanics, Applied categories.

Analysis Of Turbulent Flows With Computer Programs

DOWNLOAD
Author : Tuncer Cebeci
language : en
Publisher: Butterworth-Heinemann
Release Date : 2013-02-26

Analysis Of Turbulent Flows With Computer Programs written by Tuncer Cebeci and has been published by Butterworth-Heinemann this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-02-26 with Computers categories.

Analysis of Turbulent Flows is written by one of the most prolific authors in the field of CFD. Professor of Aerodynamics at SUPAERO and Director of DMAE at ONERA, Professor Tuncer Cebeci calls on both his academic and industrial experience when presenting this work. Each chapter has been specifically constructed to provide a comprehensive overview of turbulent flow and its measurement. Analysis of Turbulent Flows serves as an advanced textbook for PhD candidates working in the field of CFD and is essential reading for researchers, practitioners in industry and MSc and MEng students. The field of CFD is strongly represented by the following corporate organizations: Boeing, Airbus, Thales, United Technologies and General Electric. Government bodies and academic institutions also have a strong interest in this exciting field. - An overview of the development and application of computational fluid dynamics (CFD), with real applications to industry - Contains a unique section on short-cut methods – simple approaches to practical engineering problems

Advances In Heat Transfer

DOWNLOAD
Author :
language : en
Publisher: Academic Press
Release Date : 1965-01-01

Advances In Heat Transfer written by and has been published by Academic Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965-01-01 with Science categories.

Advances in Heat Transfer

The Effect Of Blade Section Thickness Ratios On The Aerodynamic Characteristics Of Related Full Scale Propellers At Mach Numbers Up To 0 65

DOWNLOAD
Author : A. J. Eggers
language : en
Publisher:
Release Date : 1953

The Effect Of Blade Section Thickness Ratios On The Aerodynamic Characteristics Of Related Full Scale Propellers At Mach Numbers Up To 0 65 written by A. J. Eggers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aerodynamics, Supersonic categories.