Safeer Hussain (Former)
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- 2021
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Mark
Endwall film cooling holes design upstream of the leading edge of a turbine vane
(
- Contribution to journal › Article
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Mark
Experimental and numerical investigations of heat transfer and fluid flow in a rectangular channel with perforated ribs
(
- Contribution to journal › Article
- 2020
-
Mark
Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane
(
- Contribution to journal › Article
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Mark
Design of Full-Scale Endwall Film Cooling of a Turbine Vane
(
- Contribution to journal › Article
- 2019
-
Mark
Heat transfer enhancement and turbulent flow in a rectangular channel using perforated ribs with inclined holes
(
- Contribution to journal › Article
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Mark
Suppression of endwall heat transfer in the junction region with a symmetric airfoil by a vortex generator pair
(
- Contribution to journal › Article
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Mark
Large eddy simulation of turbulent heat transfer in a non-isothermal channel : Effects of temperature-dependent viscosity and thermal conductivity
(
- Contribution to journal › Article
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Mark
Effect of the relative location of a pocket cavity on heat transfer and flow structures of the downstream endwall with a symmetrical vane
(
- Contribution to journal › Article
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Mark
Thermal performance enhancement in a wedge duct with in-line pin fins combined with vortex generators
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- Contribution to journal › Article
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Mark
Experimental and Numerical Investigations of Heat Transfer related to Gas Turbine Applications
2019)(
- Thesis › Doctoral thesis (compilation)
- 2018
-
Mark
Heat transfer enhancement and turbulent flow in a high aspect ratio channel (4:1) with ribs of various truncation types and arrangements
(
- Contribution to journal › Article
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Mark
Effects of a pocket cavity on heat transfer and flow characteristics of the endwall with a bluff body in a gas turbine engine
(
- Contribution to journal › Article
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Mark
Application of fractal theory in the arrangement of truncated ribs in a rectangular cooling channel (4 : 1) of a turbine blade
(
- Contribution to journal › Article
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Mark
Reduction of heat transfer on the endwall in the upstream junction region of a symmetric airfoil with vortex generator pair
(
- Chapter in Book/Report/Conference proceeding › Paper in conference proceeding
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Mark
Effects of the location of the pocket cavity on heat transfer and flow characteristics of the endwall with a symmetrical vane
(
- Chapter in Book/Report/Conference proceeding › Paper in conference proceeding