Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF full book. Access full book title Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow by K. G. Winter. Download full books in PDF and EPUB format.
Author: K. G. Winter
Publisher:
ISBN: 9780114703332
Category :
Languages : en
Pages : 76
Get Book Here
Book Description
Author: K. G. Winter
Publisher:
ISBN: 9780114703332
Category :
Languages : en
Pages : 76
Get Book Here
Book Description
Author: Kenneth George Winter
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 13
Get Book Here
Book Description
Author: K. G. Winter
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Get Book Here
Book Description
Author: Kenneth George Winter
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 75
Get Book Here
Book Description
Author: Aeronautical Research Council
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: William A. Cassels
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 76
Get Book Here
Book Description
Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fineness ratios 7, 10, and 13 at zero angle of attack for free-stream Mach numbers of 2.00, 2.75, and 4.63 and a range of Reynolds numbers based on model length of 6 to 15 X 10(to the 6 power) with and without a roughness strip. The grit method of inducing turbulence was found to provide for a nearly complete turbulent flow over the models at the lower Mach numbers and higher Reynolds numbers considered in this study while the amount of trip drag was less than 8 percent of the model drag with transition fixed. A method of interpreting sublimation data was discussed and used and the results compared well with the impact-pressure results.
Author:
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 120
Get Book Here
Book Description
Author: Tuncer Cebeci
Publisher: Elsevier
ISBN: 0323151051
Category : Technology & Engineering
Languages : en
Pages : 423
Get Book Here
Book Description
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.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
Get Book Here
Book Description
Author: Richard D. Samuels
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 100
Get Book Here
Book Description
