Results 291 to 300 of about 95,741 (349)

Measurements in a Shock Tube of Heat-Transfer Rates at the Stagnation Point of a 1.0-inch-Diameter Sphere for Real-Gas Temperatures up to 7,900 R

, 1958
A. P. Sabol
openalex   +1 more source

Climate Change Reshapes Thermal Suitability for Dairy Cattle in Jiangsu Province (1961-2020). [PDF]

Animals (Basel)
Yang G, Liu F, Zhu G, Liu Q, Wang C, Li D, Guo Z, Zhao H.   +7 more
europepmc   +1 more source

Modeling of Aerobrake Ballute Stagnation Point Temperature and Heat Transfer to Inflation Gas

, 2013
Parviz A. Bahrami
openalex   +1 more source

Fingerprint of Droplet Shape and Vortex in the Line Shape at the Electronic Band Origin of Phthalocyanine in Superfluid Helium Droplets. [PDF]

ACS Phys Chem Au
Jagode RPM, Scrimgeour A, Schlaghaufer F, Fischer J, Slenczka A.   +4 more
europepmc   +1 more source

Optimization of proton exchange membrane fuel cell design parameters using Tianji's horse racing optimization. [PDF]

Sci Rep
Bouali Y, Imarazene K, Alamri B, Berkouk EM.   +3 more
europepmc   +1 more source

Acceleration of butane vapor nucleation by carbon dioxide gas.

Phys Chem Chem Phys
Choudhury A, Graber F, Feusi S, Krohn J, Khatri J, Hernandez FT, Li C, Signorell R.   +7 more
europepmc   +1 more source

Granulomatous Lobular Mastitis: A Rare Case of Erythema Nodosum.

Indian J Dermatol
Xi Y, Zheng R, He Z, Dong Q.
europepmc   +1 more source

Some of the next articles are maybe not open access.

Related searches:

A representation for the temperature field near the stagnation region in oblique stagnation flow

Physics of Fluids A, Fluid Dynamics, 1990
Oblique stagnation flow has been the subject of previous work. In this Brief Communication, attention is restricted to the case in which the flow is steady, inviscid, and two dimensional. A general solution to the thermal field valid in the region of the stagnation point, which formally exhibits x dependence, is sought.
exaly   +2 more sources

A General Expression for the Isentropic Stagnation Temperature of a Fluid

Nature, 1964
THE 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.
exaly   +2 more sources

An Unusual Aerodynamic Stagnation-Temperature Effect

Journal of the Aerospace Sciences, 1959
Irvin Glassman
exaly   +2 more sources