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transport terrestre - iate.europa.eu
transport terrestre - iate.europa.eu
New correlations for the air-side heat transfer coefficient of microchannel heat exchangers under quasi-steady state frosting operating conditions... A set of empirical correlations were developed to predict the frost thickness on fin leading edge and the reduction of air face velocity due to air pressure drop across the frosted coil during frosting operation....
général - core.ac.uk - PDF: docs.lib.purdue.edu
Numerical study of three-dimensional separation and flow control at a wing/body junction... Fillets with a radius of three and one-half times the fin leading edge diameter or two times the incoming boundary layer thickness, significantly weaken the usual necklace interaction vortex for the Mach number and Reynolds number...
Shuttle ascent and shock impingement aerodynamic heating studies... The data were categorized into four interference areas; fin leading edge, wing/fuselage fin/plate corners, and space shuttle configurations....
Experimental investigation of shock-shock interactions over a 2-d wedge at m=6The effects of fin-leading-edge radius and sweep angle on peak heating rates due to shock-shock interactions were investigated in the NASA Langley Research Center 20-inch Mach 6 Air Tunnel....
Global aeroheating measurements of shock-shock interactions on a swept cylinderThe effects of fin leading-edge radius and sweep angle on peak heating rates due to shock-shock interactions were investigated in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel....


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