R
Ravish Vinze
Researcher at Defence Institute of Advanced Technology
Publications - 9
Citations - 154
Ravish Vinze is an academic researcher from Defence Institute of Advanced Technology. The author has contributed to research in topics: Nusselt number & Heat transfer. The author has an hindex of 7, co-authored 9 publications receiving 106 citations.
Papers
More filters
Journal ArticleDOI
Influence of jet temperature and nozzle shape on the heat transfer distribution between a smooth plate and impinging air jets
TL;DR: In this article, the effects of nozzle shape, jet temperature and nozzle to distance (z/de) on heat transfer distribution due to impingement of air jet on a smooth flat plate were investigated.
Journal ArticleDOI
Local heat transfer distribution between smooth flat surface and impinging incompressible air jet from a chevron nozzle
TL;DR: In this paper, the influence of chevron nozzle on local heat transfer distribution over a flat plate impinged by incompressible jets is studied for Reynolds numbers of 28,000, 35,000 and 40,000.
Journal ArticleDOI
Effect of dimple pitch and depth on jet impingement heat transfer over dimpled surface impinged by multiple jets
TL;DR: In this paper, the effect of dimpled surface configurations on heat transfer was investigated for multiple jets issuing from orifices arranged in a 3'×'3' array, where the distance between the orifice plate and the test surface is varied from 1d to 6d.
Journal ArticleDOI
Influence of the shape of the orifice on the local heat transfer distribution between smooth flat surface and impinging incompressible air jet
TL;DR: In this paper, the influence of the shape of the orifice (circular, square, triangular and elliptical), jet to plate distances and Reynolds number on the local heat transfer distribution to normally impinging submerged air jet on smooth and flat surface was investigated.
Journal ArticleDOI
Influence of the orifice shape on the local heat transfer distribution and axis switching by compressible jets impinging on flat surface
TL;DR: In this paper, the effects of the orifice shape and Mach number (M) on the local heat transfer distribution by normally impinging compressible jets were investigated. And the authors measured the heat transfer by thin foil IR technique for different nozzle to plate distances.