Summary of Available Information on Reynolds Analogy for Zero-pressure-gradient, Compressible, Turbulent-boundary-layer 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 Summary of Available Information on Reynolds Analogy for Zero-pressure-gradient, Compressible, Turbulent-boundary-layer Flow PDF full book. Access full book title Summary of Available Information on Reynolds Analogy for Zero-pressure-gradient, Compressible, Turbulent-boundary-layer Flow by Aubrey M. Cary. Download full books in PDF and EPUB format.
Author: Aubrey M. Cary
Publisher:
ISBN:
Category : Reynolds analogy
Languages : en
Pages : 28
Get Book Here
Book Description
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary layer flow in adiabatic conditions.
Author: Aubrey M. Cary
Publisher:
ISBN:
Category : Reynolds analogy
Languages : en
Pages : 28
Get Book Here
Book Description
Mathematical analysis of Reynolds analogy for turbulent heat transfer, skin friction, and boundary layer flow in adiabatic conditions.
Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 580
Get Book Here
Book Description
Author: Neal Tetervin
Publisher:
ISBN:
Category : Enthalpy
Languages : en
Pages : 96
Get Book Here
Book Description
The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient. The Crocco relation between the velocity and total enthalpy for a non-adiabatic surface and zero pressure gradient is generalized to non-zero pressure gradient. The relation between the velocity and the total enthalpy varies markedly from the flat plate Crocco relation as the pressure gradient departs from zero. The magnitude of the variation depends on the velocity profile shape parameter. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 684
Get Book Here
Book Description
Author: Richard D. Samuels
Publisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Jet propulsion
Languages : en
Pages : 120
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 700
Get Book Here
Book Description
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.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 780
Get Book Here
Book Description
Author: Robert L. P. Voisinet
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 128
Get Book Here
Book Description
The results of a detailed experimental investigation of the compressible turbulent boundary layer in a zero-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall for a nominal Mach number of 4.9, at momentum thickness Reynolds numbers from 7,000. to 58,000. and at wall-to-adiabatic-wall temperature ratios of 1.0, 0.8 and 0.25. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. Furthermore, the wall shear and surface heat transfer were measured directly with a skin-friction balance and a heat-transfer gage, respectively. (Author Modified Abstract).
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 568
Get Book Here
Book Description
