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Keywords: tip clearance
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Proceedings Papers
Proc. ASME. GTINDIA2021, ASME 2021 Gas Turbine India Conference, V001T04A006, December 2–3, 2021
Paper No: GTINDIA2021-76013
.... The parametric analysis was carried out on splitter blade placement, wrap angle (10°, 20°, 30°, and 50°), and exit cone angle (30°, 40°, 50°, 60°, and 65°), at constant tip clearance and keeping the other parameters constant to observe their effect on performance and flow structure. The use of splitter blades...
Proceedings Papers
Proc. ASME. GTINDIA2019, Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics, V001T02A023, December 5–6, 2019
Paper No: GTINDIA2019-2663
... as turbulence intensity is changed to 10%. annular turbine cascade CFD secondary flow tip clearance LPT NUMERICAL STUDY OF PART CLEARANCE AND FREE STREAM TURBULENCE ON HIGH END-WALL LP TURBINE NOZZLE ANNULAR CASCADE Hardikkumar Bhavsar, Chetan S. Mistry Department of Aerospace Engineering, Indian...
Proceedings Papers
Proc. ASME. GTINDIA2019, Volume 1: Compressors, Fans, and Pumps; Turbines; Heat Transfer; Structures and Dynamics, V001T01A012, December 5–6, 2019
Paper No: GTINDIA2019-2622
..., the influence of the change of the gap on the total pressure ratio and the efficiency curve was studied when the state of the hub is fixed. Then, the influence of the rotation of the hub on the total pressure ratio and the efficiency curve was discussed when the tip clearance is fixed. Finally, the total...
Proceedings Papers
Proc. ASME. GTINDIA2013, ASME 2013 Gas Turbine India Conference, V001T02A006, December 5–6, 2013
Paper No: GTINDIA2013-3568
... This paper deals with the numerical investigations on a low pressure axial turbine stage to assess the effect of variation in rotor tip clearance and tip coolant ejection rate on the end wall losses. The rotor, along with the NGV, was modeled to represent the entire turbine stage. The CFX...
Proceedings Papers
Proc. ASME. GTINDIA2012, ASME 2012 Gas Turbine India Conference, 115-121, December 1, 2012
Paper No: GTINDIA2012-9571
... 1 Copyright © 2012 by ASME CFD CODE VALIDATION & QUALITATIVE STUDY OF EFFECTS OF TIP CLEARANCE VARIATION ON PERFORMANCE OF TRANSONIC AXIAL COMPRESSOR ROTOR Aniket R.Patkar Sardar Patel College of Engineering Mumbai, Maharashtra, India Email: aniketpatkar87@gmail.com Srinivethan Rangasamy Zeus...
