Analysis of Heat Transfer, Burnout, Pressure Drop and Density Data for High-pressure Water
Author : W. H. Jens
Publisher :
Page : 146 pages
File Size : 49,90 MB
Release : 1955
Category : Heat exchangers
ISBN :
Author : W. H. Jens
Publisher :
Page : 146 pages
File Size : 49,90 MB
Release : 1955
Category : Heat exchangers
ISBN :
Author :
Publisher :
Page : pages
File Size : 19,5 MB
Release : 1951
Category :
ISBN :
Author : W. H. Jens
Publisher :
Page : 0 pages
File Size : 20,20 MB
Release : 1951
Category :
ISBN :
Author : W. R. Gambill
Publisher :
Page : 118 pages
File Size : 30,33 MB
Release : 1960
Category : Fluid dynamics
ISBN :
Author : W. R. Gambill
Publisher :
Page : 122 pages
File Size : 23,61 MB
Release : 1960
Category : Fluid dynamics
ISBN :
Author : R. A. DeBortoli
Publisher :
Page : 192 pages
File Size : 31,86 MB
Release : 1958
Category :
ISBN :
Author : U.S. Atomic Energy Commission
Publisher :
Page : 328 pages
File Size : 10,91 MB
Release : 1957
Category : Heat
ISBN :
Author : Paul D. Roach
Publisher :
Page : 33 pages
File Size : 18,42 MB
Release : 1989
Category :
ISBN :
Author : R. K. Shah
Publisher : CRC Press
Page : 1104 pages
File Size : 26,52 MB
Release : 1988-07-01
Category : Science
ISBN : 9780891167297
Author : Albert D. Hemenover
Publisher :
Page : 764 pages
File Size : 16,34 MB
Release : 1954
Category : Aerofoils
ISBN :
The effects of variation of trailing-edge angle and trailing-edge thickness on the lift characteristics of a 10-percent-chord thick symmetrical NACA airfoil section with a 25-percent-chord plain flap are appraised from wind-tunnel tests at Mach numbers from 0.3 to 0.9 and Reynolds numbers varying correspondingly from 1 to 2 million. The airfoil trailing-edge angle was varied from approximately 18 to 6 degrees, and the trailing-edge thickness from zero to the thickness at the flap hinge line.