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Temperature-dependent heat sources or sinks in a stagnation point flow
Applied Scientific Research, 1961An analytical study has been made to determine the heat transfer characteristics of a stagnation point flow in which there are temperature-dependent heat sources or sinks. Results have been obtained for both strong and weak sources or sinks for a Prandtl number of 0.7.
Sparrow, E. M., Cess, R. D.
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Temperature-dependent collector properties from stagnation measurements
Solar Energy, 1980J.M. Gordon, D. Govaer, Y. Zarmi
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An Unusual Aerodynamic Stagnation-Temperature Effect
Journal of the Aerospace Sciences, 1959Irvin Glassman, James E. A. John
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A General Expression for the Isentropic Stagnation Temperature of a Fluid
Nature, 1964THE stagnation temperature of a fluid is commonly represented by the expression: where T, U and cp denote the temperature, velocity and specific heat at constant pressure, and the subscripts 0 and ∞ refer to the stagnation point and free stream, respectively.
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Stagnation Temperature Control in Blowdown Wind Tunnels
Journal of the Aerospace Sciences, 1958J. S. MURPHY +2 more
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A Heated Hypersonic Stagnation-Temperature Probe
Journal of the Aerospace Sciences, 1960openaire +1 more source
Stagnation temperature and molecular weight effects in jet interaction
AIAA Journal, 1970R. A. CHAMBERS, D. J. COLLINS
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REDUCTION OF STAGNATION TEMPERATURES IN EVACUATED TUBULAR COLLECTORS
1988R.E. Collins, B.A. Pailthorpe, S. O'Shea
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Temperature Distribution in Laminar Stagnation-Point Flow with Axisymmetry
Journal of the Aeronautical Sciences, 1954openaire +2 more sources
Stagnation Temperature Effect on the Prandtl Meyer Function
AIAA Journal, 2007openaire +1 more source