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Keywords: transonic flow
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2025, 147(4): 041002.
Paper No: TURBO-24-1071
Published Online: October 25, 2024
... 09 2024 20 09 2024 25 10 2024 Graphical Abstract Figure meanline model off-design transonic flow Lagrange multipliers critical flow EEA Grants 10.13039/501100007048 TO01000160 TO01000160 Research Executive Agency 10.13039/501100000783 899987...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2025, 147(3): 031001.
Paper No: TURBO-24-1085
Published Online: October 8, 2024
... Graphical Abstract Figure compressor supersonic through-flow variable-pitch tandem fan CFD transonic flow supersonic flow computational fluid dynamics (CFD) fan compressor and compressor aerodynamic design fluid dynamics and heat transfer phenomena in compressor and turbine components...
Journal Articles
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2012, 134(4): 041022.
Published Online: July 25, 2011
...-Stokes equations rotors subsonic flow transonic flow turbines turbulence 02 11 2010 12 09 2010 25 07 2011 25 07 2011 This section provides a brief description of the pertinent numerical details related to this work. Further information can be found in Refs. 2 12...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2012, 134(3): 031020.
Published Online: July 15, 2011
... known as boundary-layer-ingesting (BLI) inlet. aerospace components aircraft boundary layer turbulence flow control Navier-Stokes equations transonic flow 06 07 2010 02 08 2010 15 07 2011 15 07 2011 Representative B-spline patch used to parameterize...
Journal Articles
Journal Articles
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041027.
Published Online: April 27, 2011
... 22 07 2010 27 04 2011 27 04 2011 blades computational fluid dynamics heat transfer Mach number shock waves transonic flow The tip of an unshrouded turbine rotor blade is one of the most vulnerable areas on turbine blade due to its high thermal load and difficulty...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041025.
Published Online: April 26, 2011
...: An Experimental Investigation ,” ASME J. Turbomach. 0889-504X , 120 , pp. 530 – 540 . 11 02 2010 22 02 2010 26 04 2011 26 04 2011 blades boundary layer turbulence bubbles computational fluid dynamics cooling heat transfer Mach number transonic flow turbines...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041001.
Published Online: April 19, 2011
...Q. Zhang; D. O. O’Dowd; L. He; A. P. S. Wheeler; P. M. Ligrani; B. C. Y. Cheong In this paper, the transonic flow pattern and its influence on heat transfer on a high-pressure turbine blade tip are investigated using experimental and computational methods. Spatially resolved heat transfer data...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2011, 133(3): 031030.
Published Online: February 28, 2011
... 01 2010 28 02 2011 28 02 2011 blades computational fluid dynamics design engineering gas turbines heat transfer rotors stators transonic flow turbulence Combustion chamber exit mean temperature values have increased considerably to allow higher efficiency...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2011, 133(3): 031014.
Published Online: November 16, 2010
... computational fluid dynamics design engineering Navier-Stokes equations optimisation plastic flow transonic flow turbines Shape design optimization in aerodynamics is an approach to obtain the geometric shape following the given criteria of aerodynamic performance with both geometric...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2011, 133(2): 021014.
Published Online: October 22, 2010
... flow instability rotors transonic flow Therefore, a conclusion can be reached: Peak efficiency and stall margin each has a nonlinear functional relationship with the excitation frequency of the casing treatment. Meanwhile, the optimal excitation frequency for efficiency (maximum peak...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2011, 133(2): 021010.
Published Online: October 21, 2010
... of inlet stagnation pressure profile for different amplitudes of inlet nonuniformity 20 07 2009 20 08 2009 21 10 2010 21 10 2010 blades compressors flow instability rotors stagnation flow transonic flow vortices wakes The design of highly loaded, high Mach...