INVESTIGATION OF TURBINE BLADE FILM COOLING WITH CHANGE IN SHAPE AND ORIENTATION (original) (raw)
EFFECT OF HOLE -SHAPED ON FILM COOLING EFFECTIVENESS OF GAS TURBINE BLADE
Ahmed Helal
IECEC-2012-1283396, 2012
View PDFchevron_right
Numerical Investigation of Film Cooling Effectiveness in Turbine Blades
a k ROY
View PDFchevron_right
Numerical simulation on film cooling with compound angle of blade leading edge model for gas turbine
Zhenan Zhao
International Journal of Heat and Mass Transfer, 2017
View PDFchevron_right
A numerical investigation of new film cooling hole configuration at the leading edge of asymmetrical turbine blade: part A
mustapha benabed
Heat and Mass Transfer, 2012
View PDFchevron_right
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes
Meinhard Schobeiri
International Journal of Heat and Mass Transfer, 2007
View PDFchevron_right
Maximization of Cooling Effectiveness of Turbine Blade Surfaces Using Different Arrangement of Cooling Holes and Various Blowing Ratios
Prakhar Jindal
2018
View PDFchevron_right
Progress Of Film Cooling In Industrial Gas Turbine Vanes And Blades
Kenichiro Takeishi
2017
View PDFchevron_right
Heat Transfer Simulation of Gas Turbine Blade with Film Cooling
Khaled Al-Farhany
International Journal of Modern Engineering and Research Technology, 2018
View PDFchevron_right
NUMERICAL SIMULATION TO INVESTIGATE EFFECT OF DOWNSTREAM GROOVES ON FILM COOLING EFFECTIVENESS OF GAS TURBINE BLADES
IAEME Publication
View PDFchevron_right
Recent Development in Turbine Blade Film Cooling
Srinath Ekkad
International Journal of Rotating Machinery, 2001
View PDFchevron_right
A COMPARATIVE STUDY OF THE FILM COOLING HOLE CONFIGURATION EFFECTS ON THE LEADING EDGE OF ASYMMETRICAL TURBINE BLADE
mustapha benabed
ichmt.org
View PDFchevron_right
Influence of leading-edge lateral injection angles on the film cooling effectiveness of a gas turbine blade
Bassam Jubran
Heat and Mass Transfer, 2004
View PDFchevron_right
Effect of Hole Blockage Configurations on Film Cooling in Gas Turbine Components
η θΏ, Dr. GUELAILIA Ahmed
View PDFchevron_right
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF ADIABATIC FILM COOLING EFFECTIVENESS OVER THE COMPOUND ANGLED GAS TURBINE BLADE LEADING EDGE MODEL
IAEME Publication
View PDFchevron_right
Numerical approach to new tangential slot effect on film cooling effectiveness over asymmetrical turbine blade
mustapha benabed
View PDFchevron_right
Effect of hole stream wise angle in flat plate, pressure side (concave) and suction side (convex) on film cooling effectiveness
Ahmed Helal
1st Aviation Engineering Innovations Conference AEIC -2015-000, 2015
View PDFchevron_right
THERMAL ANALYSIS OF COOLING EFFECT ON GAS TURBINE BLADE
Editor IJRET
View PDFchevron_right
Numerical investigation on film cooling of gas turbine blade using anti-vortex holes
Sai Sanjay S
INTERNATIONAL CONFERENCE ON ADVANCES IN MATERIALS, COMPUTING AND COMMUNICATION TECHNOLOGIES: (ICAMCCT 2021), 2022
View PDFchevron_right
Effect of cooling passage imperfection on the flow characteristics of film-cooled gas turbine blade
D Raja Joseph
International Journal of Ambient Energy, 2018
View PDFchevron_right
A210 Experimental and Numerical Studies on Leading Edge Film Cooling of a HP Turbine Blade Model(Gas Turbine-6)
Hamidon Bin Salleh
The Proceedings of the International Conference on Power Engineering (ICOPE), 2009
View PDFchevron_right
Effect of Film-Hole Shape on Turbine-Blade Film-Cooling Performance
Je-chin Han
Journal of Thermophysics and Heat Transfer, 2001
View PDFchevron_right
Analysis of combined convective and film cooling on an existing turbine blade
S. Woldendorp
View PDFchevron_right
EFFECTS OF MASS FLOW RATE ON FILM COOLING EFFECTIVENESS OF GAS TURBINE BLADES INTERNATIONAL CONGRES ON MATERIALS AND ENERGY CIMATEN2014 EFFECTS OF MASS FLOW RATE ON FILM COOLING EFFECTIVENESS OF GAS TURBINE BLADES
Dr. GUELAILIA Ahmed
View PDFchevron_right
Finite Volume Based Numerical Investigation On The Effects Of Internal Cooling And Film Cooling On The Thermal Performance Of Gas Turbine Blades
sufian shaker
2010
View PDFchevron_right
Recent studies in turbine blade cooling
Ali Alkathemy
International Journal of Rotating Machinery, 2004
View PDFchevron_right
ON THE CALCULATIONS OF FLAT PLATE FILM COOLING EFFECTIVENESS
Ahmed Helal
IECEC-2012-1283396, 2012
View PDFchevron_right
Numerical analysis on the film cooling of leading edge with laid back holes to determine the optimal angle for the holes
Ali Solati
Australian journal of mechanical engineering, 2018
View PDFchevron_right
The effect of jet angle and velocity ratio on turbine blade film cooling
Muna S . Kassim
WIT transactions on modelling and simulation, 2013
View PDFchevron_right
Numerical Analysis of Film Cooling Effectiveness under Variable Blowing Ratio and Injection Angles
Mehmet F Orhan
Proceedings of the 3rd World Congress on Momentum, Heat and Mass Transfer, 2018
View PDFchevron_right
Numerical Analysis of Film Cooling Due to Simple/Compound Angle Hole Combination
Ahamed C
Arabian Journal for Science and Engineering, 2020
View PDFchevron_right
Cooling of Rotating Turbine Blades β A Novel Approach
Kaushik Kumar
2020
View PDFchevron_right
IJERT-Heat Transfer Analysis of Gas Turbine Rotor Blade Cooling Through Staggered Holes using CFD
IJERT Journal
International Journal of Engineering Research and Technology (IJERT), 2015
View PDFchevron_right