Film Cooling From a Row of Holes Supplemented With Antivortex Holes (original) (raw)

Effect of Pressure Gradient on Film Cooling From Holes Supplemented by Anti-Vortex Holes

tarek Meakhail

International Conference on Aerospace Sciences and Aviation Technology

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Film Cooling Effectiveness from Single and Two Inlined/ Staggered Rows of Novel Semicircular Cooling Holes

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Mehran University Research Journal of Engineering and Technology, 2012

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Development of a novel film cooling hole geometry

Jane Sargison

2001

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Effect Of Hole Shapes, Orientation And Hole Arrangements On Film Cooling Effectiveness

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Effect of Multi-hole Configuration on Film Cooling Effectiveness

AUT Journal of Mechanical Engineering

2019

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THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS 94@BULLETGT@BULLET312 FILM COOLING WITH COMPOUND ANGLE HOLES: ADIABATIC EFFECTIVENESS

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Film Cooling from a Single Row of Compound Angle Holes at High Blowing Ratios

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Study on the Thermal and Flow Fields of Shaped Film-Cooling Holes

Kenichiro Takeishi

Heat transfer research, 2011

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Film Cooling from Two Staggered Rows of Compound Angle Holes at High Blowing Ratios

Phillip Ligrani

International Journal of Rotating Machinery, 1996

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Film cooling effectiveness from trenched shaped and compound holes

Bassam Jubran, sima baheri

Heat and Mass Transfer, 2008

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Numerical Investigation of Film Cooling from Two Rows of Holes with Anti-Vortex Holes Attached to the Upstream Row

Zeitgeist David

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A numerical investigation of film cooling performance through variations in the location of discrete sister holes

Siavash Khajehhasani

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Experimental assessment of film cooling performance of short cylindrical holes on a flat surface

M. Ravi, Dr. Kuldeep Singh

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Influence of mainstream flow history on film cooling and heat transfer from two rows of simple and compound angle holes in combination

Bassam Jubran

International Journal of Heat and Fluid Flow, 1999

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A Review of Hole Geometry and Coolant Density Effect on Film Cooling

Je-chin Han

Frontiers in Heat and Mass Transfer, 2015

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Effects of pressure gradient on film cooling effectiveness from two rows of simple and compound angle holes in combination

Bassam Jubran

Energy Conversion and Management, 2004

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Numerical Analysis of Film Cooling Due to Simple/Compound Angle Hole Combination

Ahamed C

Arabian Journal for Science and Engineering, 2020

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Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation

Emily Boyd

2014

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Improved film cooling from cylindrical angled holes with triangular tabs: effect of tab orientations

Srinath Ekkad

International Journal of Heat and Fluid Flow, 2003

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Experimental Investigation of Film Cooling Performance for a New Shaped Hole at the Leading Edge

Ibrahim Hassan

Volume 2: Simple and Combined Cycles; Advanced Energy Systems and Renewables (Wind, Solar and Geothermal); Energy Water Nexus; Thermal Hydraulics and CFD; Nuclear Plant Design, Licensing and Construction; Performance Testing and Performance Test Codes; Student Paper Competition, 2014

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EFFECT OF COOLANT JET HOLES ARRANGEMENT ON FILM COOLING PERFORMANCE

IJESRT Journal

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Effects of the laidback fan-shaped hole geometry on film cooling performance using large eddy simulation

Hakun Jang

Proceeding of 5th Thermal and Fluids Engineering Conference (TFEC)

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Film cooling from a single row of holes oriented in spanwise/normal planes

Phillip Ligrani

1997

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Flowfield Measurements for Film-Cooling Holes With Expanded Exits

Karen Thole

1996

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Film Cooling From Spanwise-Oriented Holes in Two Staggered Rows

Phillip Ligrani

Journal of Turbomachinery, 1997

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Numerical modelling of film cooling from converging slot-hole

Bassam Jubran

Heat and Mass Transfer, 2006

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Computations of Film Cooling From Holes With Struts

Minking Chyu

Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration

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The Effects of Row Trench Holes with Alignment Angle of +60 Degrees on Film Cooling Effectiveness at Low Blowing Ratios

Ehsan Kianpour

2014

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EFFECTS OF BLOWING RATIO ON THE HEAT TRANSFER COEFFICIENT DISTRIBUTION DOWNSTREAM OF A SINGLE FILM COOLING HOLE

Abd Al-Nasir

2006

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An Investigation of the Effect of Anti-Vortex Film Cooling On a Flat Plate

Samir Ayad

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FILM COOLING EFFECTIVENESS FOR DIFFERENT HOLE SHAPES AND BLOWING RATIOS

Prakhar Jindal

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The Effect of Freestream Turbulence on Film Cooling Heat Transfer Coefficient and Adiabatic Effectiveness Using Compound Angle Holes

James E Mayhew

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