Results 161 to 170 of about 159,512 (193)
Some of the next articles are maybe not open access.
ZAMP Zeitschrift f�r angewandte Mathematik und Physik, 1994
This paper is concerned with the extension of the theory of vortex breakdown, that was presented in previous publications by the present author and others, to cases of non-uniform density and non-uniform stagnation pressure outside the vortex core. The effects of radial density and velocity variations play an essential role for the layout of modern low-
openaire +3 more sources
This paper is concerned with the extension of the theory of vortex breakdown, that was presented in previous publications by the present author and others, to cases of non-uniform density and non-uniform stagnation pressure outside the vortex core. The effects of radial density and velocity variations play an essential role for the layout of modern low-
openaire +3 more sources
High-pressure combustion characteristics of liquid fuel in the stagnation-point flow
Symposium (International) on Combustion, 1992Combustion and vaporization of liquid fuels, under high pressure were investigated in the stagnation-point flow field. The diffusion flame was established slightly above the liquid heptane pool parallel to the surface, and the combustion mass flux was measured at various pressures up to 3.5 MPa.
Naomichi Ono +2 more
openaire +2 more sources
Stagnation pressure effect on the supersonic minimum length nozzle design
The Aeronautical Journal, 2019ABSTRACTThe aim of this work is to develop a calculation model based on the method of characteristics making it possible to study the effect of the stagnation pressure of the combustion chamber on the 2D and axisymmetric minimum length nozzle design giving a uniform and parallel flow at the exit section.
openaire +2 more sources
Shock Oscillations in a Supersonic Diffuser Flow with Varying Stagnation Pressure
2019The flow in supersonic wind tunnel diffusers is usually transonic in nature, and the formation of a normal shock just downstream of the diffuser throat region is required for power economy. The behavior of this starting normal shock decides the start or unstarts of a supersonic wind tunnel.
Jintu K. James, T. M. Muruganandam
openaire +2 more sources
Pressure-tailored lithium deposition and dissolution in lithium metal batteries
Nature Energy, 2021Chengcheng Fang, Bingyu Lu, Gorakh Pawar
exaly
Accuracy in Computational Aerodynamics Part 1: Stagnation Pressure
SAE Technical Paper Series, 1998Niklas Axelsson +2 more
openaire +2 more sources
Impact of Outlet Restriction on RDC Performance and Stagnation Pressure Rise [PDF]
AIAA Scitech 2019 Forum, 2019 Myles D. Bohon +3 more
openaire +1 more source
Rise of Total Pressure Near the Stagnation Point on a Sphere
AIAA Journal, 2002openaire +2 more sources