Results 271 to 280 of about 12,079 (285)

An Unusual Aerodynamic Stagnation-Temperature Effect

Journal of the Aerospace Sciences, 1959
Irvin Glassman, James E. A. John
openaire   +2 more sources

Design and Calibration of Stagnation Temperature Probes for Use at High Supersonic Speeds and Elevated Temperatures

Journal of Applied Physics, 1954
A stagnation temperature probe with a single platinum-coated silica shield was built for use at high supersonic speeds and elevated temperatures. For large Reynolds numbers the temperature recovery factor of the probe reaches 0.998. It decreases with decreasing Reynolds number and increasing temperature.
openaire   +2 more sources

Temperature diagnostics in the hypersonic flow regime - An application to develop a stagnation temperature probe [PDF]

International Aerospace Planes and Hypersonics Technologies, 1995
O. Pin, Jean-Marie Badie, G Olalde, M Clement   +3 more
openaire   +1 more source

Stagnation Temperature Control in Blowdown Wind Tunnels

Journal of the Aerospace Sciences, 1958
J. S. Murphy, Duncan Rannie, G. W. Timson   +2 more
openaire   +2 more sources

Temperature-dependent collector properties from stagnation measurements

Solar Energy, 1980
Yair Zarmi, D. Govaer, Jeffrey M. Gordon
openaire   +2 more sources

A Heated Hypersonic Stagnation-Temperature Probe

Journal of the Aerospace Sciences, 1960
openaire   +2 more sources

Stagnation Temperature Effect on the Prandtl Meyer Function

AIAA Journal, 2007
openaire   +2 more sources

Comment on "Stagnation Temperature Effect on the Prandtl Meyer Function"

AIAA Journal, 2007
openaire   +2 more sources

Temperature Distribution in Laminar Stagnation-Point Flow with Axisymmetry

Journal of the Aeronautical Sciences, 1954
openaire   +2 more sources

Experimental Study of the Stagnation Temperature in a Free Molecular Flow

Journal of the Aeronautical Sciences, 1957
openaire   +2 more sources