The Effect of Blowing Ratio on Film Cooling Effectiveness Using Cylindrical and Row Trenched Cooling Holes with Alignment Angle of 90 Degrees

The Effect of Blowing Ratio on Film Cooling Effectiveness Using Cylindrical and Row Trenched Cooling Holes with Alignment Angle of 90 Degrees

Bibliographic Details
Main Authors:	Nor Azwadi, Ehsan Kianpour
Format:	Article
Language:	English
Published:	Hindawi Limited 2014-01-01
Series:	Mathematical Problems in Engineering
Online Access:	http://dx.doi.org/10.1155/2014/470576

Similar Items

Computational investigation of film cooling from cylindrical and row trenched cooling holes near the combustor endwall
by: Ehsan Kianpour, et al.
Published: (2014-11-01)

Computational investigation of film cooling from cylindrical and row trenched cooling holes near the combustor end wall
by: Kianpour, Ehsan, et al.
Published: (2014)

A detailed study of effects of row trenched holes at the combustor exit on film cooling effectiveness
by: Kianpour, Ehsan, et al.
Published: (2017)

A detailed study of row-trenched holes at the combustor exit on film-cooling effectiveness
by: Kianpour, E., et al.
Published: (2019)

Film Cooling from Two Staggered Rows of Compound Angle Holes at High Blowing Ratios
by: Phillip M. Ligrani, et al.
Published: (1996-01-01)

Film Cooling from a Single Row of Compound Angle Holes at High Blowing Ratios
by: Phillip M. Ligrani, et al.
Published: (1996-01-01)

Effects of hole arrangement and trenched hole on multirow film cooling
by: Cui, J., et al.
Published: (2022)

Film cooling effectiveness in a gas turbine engine: a review
by: Kianpour, Ehsan, et al.
Published: (2014)

Film cooling from rows of discrete holes
by: Saluja, C. L.
Published: (1977)

Film Cooling Effectiveness from Single and Two Inlined/ Staggered Rows of Novel Semicircular Cooling Holes
by: Fayyaz Hussain Asghar, et al.
Published: (2012-04-01)

MAXIMIZATION OF COOLING EFFECTIVENESS OF TURBINE BLADE SURFACES USING DIFFERENT ARRANGEMENT OF COOLING HOLES AND VARIOUS BLOWING RATIOS
by: MADHURIMA DEY, et al.
Published: (2018-04-01)

Heat transfer, adiabatic effectiveness and injectant distributions downstream of single rows and two staggered rows of film-cooling holes with simple and compound angles.
by: Jackson, Stephen Mark
Published: (2013)

Heat transfer, adiabatic effectiveness and injectant distributions downstream of single and double rows of film-cooling holes with compound angles
by: Bishop, David Turner
Published: (2013)

Heat transfer, adiabatic effectiveness and injectant distribution downstream of single and double rows of film-cooling holes with compound angles.
by: Wigle, James Michael
Published: (2013)

The cooling performance of three-row compound angle holes on the suction surface of a rotating turbine blade
by: Zhiyu Zhou, et al.
Published: (2021-03-01)

Blowing Ratio Effects on Film Cooling Effectiveness
by: Liu, Kuo-Chun
Published: (2010)

Film Cooling from Cylindrical Holes in Transverse Slots
by: Altorairi, Mohammed
Published: (2003)

Film Cooling from a Row of Holes Supplemented with Anti Vortex Holes
by: Dhungel, Alok
Published: (2007)

Heat transfer, adiabatic effectiveness and injectant distributions downstream of single and double rows of film-cooling holes with simple and compound angles
by: Ciriello, Salvatore.
Published: (2013)

Numerical Investigation of Film Cooling from Two Rows of Holes with Anti-Vortex Holes Attached to the Upstream Row
by: Mostafa Abdelmohimen Hussien Abdelmohimen
Published: (2015-04-01)

Numerical Investigation of Film Cooling from Two Rows of Holes with Anti-Vortex Holes Attached to the Upstream Row
by: Mostafa Abdelmohimen Hussien Abdelmohime
Published: (2015-04-01)

Enhancing film cooling effectiveness in a gas turbine end-wall with a passive semi cylindrical trench
by: Ravi Duraisamy, et al.
Published: (2019-01-01)

Effect of vortex circulation on injectant from a single film-cooling hole and a row of film-cooling holes in a turbulent boundary layer
by: Kaisuwan, Pisut
Published: (2013)

Modeling the Effectiveness of Cooling Trenches for Stormwater Temperature Mitigation
by: Scott A. Wells
Published: (2021-01-01)

Film cooling from two rows of holes in the streamwise and spanwise directions
by: Jubran, B. A. A. Q.
Published: (1984)

Experimental research on film cooling characteristics of multi-film-hole-rows
by: Bo-lun Zhang, et al.
Published: (2021-10-01)

Effect of Hole Configurations on Film Cooling from Cylindrical Inclined Holes for the Application to Gas Turbine Blades
by: Lu, Yiping
Published: (2007)

Study on Film Cooling Performance of Round Hole Embedded in Different Shaped Craters and Trenches
by: Xiaojun Wu, et al.
Published: (2021-05-01)

Effect of Inlet Compound Angle of Backward Injection Film Cooling Hole
by: Yoon Seong Jeong, et al.
Published: (2020-02-01)

Effect of forward expansion angle on film cooling characteristics of shaped holes
by: Zhang Bo, et al.
Published: (2020-07-01)

Multi-objective optimization of three rows of film cooling holes by genetic algorithm
by: Taheri Yaser, et al.
Published: (2021-01-01)

Experimental study of the effect of a transverse trench depth on film cooling effectiveness
by: I.A. Chokhar, et al.
Published: (2021-06-01)

Effect of data center servers’ power density on the decision of using in-row cooling or perimeter cooling
by: A.M. Abbas, et al.
Published: (2021-08-01)

Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes
by: Aghasi, Paul P.
Published: (2016)

Effects of the Hole Shape and Compound Angle on Film Cooling over a Concave Surface
by: Shih, Po-Chou, et al.
Published: (1998)

Effect of vortex circulation on injectant from a single film-cooling hole and a row of film-cooling holes in a turbulent boundary layer: part 1: injection beneath the vortex downwash.
by: Craig, Douglas William
Published: (2013)

Numerical study on film cooling mechanism and characteristics of cylindrical holes with branched jet injections
by: Yu Yao, et al.
Published: (2013-03-01)

Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes
by: Klavetter, Sean Robert
Published: (2014)

Effect of Blowing Ratio on the Nusselt Number and Film Cooling Effectiveness Distributions of a Showerhead Film Cooled Blade in a Transonic Cascade
by: Guy, Ashley Ray
Published: (2014)

A study of film cooling downstream of one and two rows of holes oriented in spanwise/normal planes.
by: Ramsey, Anthony Eldorado
Published: (2012)

Cannot write session to /tmp/vufind_sessions/sess_1kptspk8po3u9baiv2t5j0t8fm