Heat-transfer and Pressure Measurements on a Concave-nose Cylinder for Mach Number Range of 2.49 to 4.44
Author :
Publisher :
Page : 26 pages
File Size : 27,2 MB
Release : 1959
Category :
ISBN :
Heat Transfer and Pressure Measurement on a 5-inch Hemispherical Concave Nose at a Mach Number of 2.0
Author : J. Thomas Markley
Publisher :
Page : 24 pages
File Size : 12,88 MB
Release : 1958
Category : Heat
ISBN :
Book Description
Abstract: The concave-nose stagnation-point heating is 40 percent of that of a hemisphere nose shape having the same diameter. At angles of attack of ℗±5© and ℗± 10© there is no increase in heating of the nose. Total pressures behind the shock were experienced up to 60© on the concave part for all angles of attack. The tests were made under sea-level conditions for a Reynolds number per foot of about 14 x 106.
Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium
Author : Richard D. Wagner
Publisher :
Page : 44 pages
File Size : 22,17 MB
Release : 1961
Category : Fluid mechanics
ISBN :
Book Description
A New Dimension, Wallops Island Flight Test Range
Author : Joseph Adams Shortal
Publisher :
Page : 808 pages
File Size : 10,20 MB
Release : 1978
Category : Aeronautics
ISBN :
Book Description
Heat-transfer and Pressure Measurements on Flat-faced Cylinders at a Mach Number of 2
Author : William E. Stoney
Publisher :
Page : 38 pages
File Size : 25,99 MB
Release : 1958
Category : Cylinders
ISBN :
Book Description
Flat-faced cylinders of 12-inch dtameter and 4-inch diameter were tested at a Mach number of 2 and sea-level conditions in the preflight jet of the Langley Pilotless Aircraft Research Station at Wallops Island, Va. Both pressure distributions and heat-transfer rates were measured.
Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Author : William E. Stoney
Publisher :
Page : 16 pages
File Size : 32,92 MB
Release : 1957
Category : Aerodynamic heating
ISBN :
Book Description
Measurements of the Surface Flows, Heat Transfer, Pressure Distribution, and Longitudinal Stability of a Mercury Capsule Model at Mach Numbers of 6.9 and 9.6
Author : Philip E. Everhart
Publisher :
Page : 66 pages
File Size : 22,91 MB
Release : 1961
Category : Aerodynamic load
ISBN :
Book Description
Heat-transfer Measurements on a Concave Hemispherical Nose with Unsteady-flow Effects at Mach Numbers of 1.98 and 4.95
Author : Morton Cooper
Publisher :
Page : 19 pages
File Size : 20,25 MB
Release : 1958
Category :
ISBN :
Book Description
Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5
Author : Thorval Tendeland
Publisher :
Page : 24 pages
File Size : 12,55 MB
Release : 1959
Category : Aerodynamic heating
ISBN :
Book Description
Aerospace Engineering Index
Author :
Publisher :
Page : 904 pages
File Size : 35,80 MB
Release : 1958
Category :
ISBN :
