Results 201 to 210 of about 85,463 (302)

Numerical Analysis of Combustion in Low Mach Number Turbulent Flows.

, 1993
Tatsuya Hasegawa
openalex   +2 more sources

Using internal air injection for fuel mixing enhancement of annular hydrogen jet behind an inclined strut in a supersonic combustor: computational study. [PDF]

Sci Rep
Bouazzi Y, Ahmed Z, Basem A, Alizadeh A, Sadeq AM, Aich W, Louhichi B, Barzegar T.   +7 more
europepmc   +1 more source

Large Eddy Simulation of low Mach number flows by a high order finite volume method - Application to a natural convection problem at engine shutdown in a turbojet

, 2016
Quentin Dubois
openalex   +1 more source

Dusty streaks on the Moon: fingerprints of multiphase flow instabilities. [PDF]

Nat Commun
Rubio JS, Rodrigues NS, Qi Y, Patel M, Gorman MT, Diaz Lopez MX, Capecelatro J, Danehy PM, Ni R.   +8 more
europepmc   +1 more source

Spatial-Frequency-Scale Variational Autoencoder for Enhanced Flow Diagnostics of Schlieren Data. [PDF]

Sensors (Basel)
Yang R, Wu H, Yang R, Wu X, Song Y, Lü M, Wang M.   +6 more
europepmc   +1 more source

A Low Mach Number Diffuse-Interface Model for Multicomponent Two-Phase Flows with Phase Change

Salar Zamani Salimi, Aritra mukherjee, Marica Pelanti, Luca Brandt   +3 more
openalex   +1 more source

On the low Mach number limit of compressible flows in exterior moving\n domains [PDF]

, 2014
Eduard Feireisl, Ondřej Kreml, Václav Mácha, Šárka Nečasová   +3 more
openalex   +1 more source

Control of flow deflection angle around the corner using microjet array. [PDF]

Sci Rep
Nakadori Y, Yuura S, Kagawa T, Urita A, Handa T.   +4 more
europepmc   +1 more source

Performance of all-speed AUSM-family schemes for DNS of low Mach number turbulent channel flow

, 2013
Shingo Matsuyama
openalex   +2 more sources

An efficient approach for calculation of pitching moment in nonlinear reduced frequency method at low Mach number transonic flows [PDF]

, 2011
Masoud Kharati Koopaee, Homayoun Emdad, Mohammad Mehdi Alishahi   +2 more
openalex   +1 more source