Determination of Supercavity Shape for Axisymmetric Cavitators at Different Non-Zero Attack Angles, Using Boundary Element Method
Rouzbeh Shafaghat(Babol Noshirvani University of Technology), A. Vahedgermi(Iran University of Science and Technology), S. M. Hosseinalipour(Iran University of Science and Technology)
Cited by 2
Related Papers
Numerical simulation of hypersonic flow over highly blunted cones with spike
|Acta Astronautica|2010|181
COMPARATIVE EVALUATION OF DIFFERENT TURBULENCE MODELS FOR CONFINED IMPINGING AND OPPOSING JET FLOWS
|Numerical Heat Transfer Part A Applications|1995|90
Flow and thermal characteristics of steady two dimensional confined laminar opposing jets: Part I. Equal jets
|International Communications in Heat and Mass Transfer|1997|58
Numerical simulation of nanofluid application in a horizontal mesh heat pipe with multiple heat sources: A smart fluid for high efficiency thermal system
|Applied Thermal Engineering|2016|53
Experimental study of formation and development of coherent vortical structures in pulsed turbulent impinging jet
|Experimental Thermal and Fluid Science|2015|40