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Keywords: aerodynamic designClose
Proc. ASME. GT2022, Volume 1: Aircraft Engine; Ceramics and Ceramic Composites, V001T01A023, June 13–17, 2022
Paper No: GT2022-82347
... by introducing the air flow at hub region to the cooling fin. Therefore, in order to better improve the thermal performance of the cooling fin, an aerodynamic design of cooling fin is proposed in this paper for better thermal management of stator end-windings. Firstly, for a certain desired power output...
Proc. ASME. GT2021, Volume 2B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing, V02BT32A007, June 7–11, 2021
Paper No: GT2021-59219
.... This work describes the aerodynamic design and experimental validation of a fully featured three-stage IP turbine, including a final row of outlet guide vanes. Experiments have been conducted in a highly engine-representative transonic rotating wind tunnel at the CTA (Centro de Tecnologías Aeronáuticas...
Sayan Ghosh, Valeria Andreoli, Govinda A. Padmanabha, Cheng Peng, Steven Atkinson, Piyush Pandita, Thomas Vandeputte, Nicholas Zabaras, Liping Wang
Proc. ASME. GT2021, Volume 9B: Structures and Dynamics — Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Structural Mechanics and Vibration, V09BT27A003, June 7–11, 2021
Paper No: GT2021-58842
... IDeAS calculates the design explicitly without costly iteration and overcomes the challenges associated with ill-posed inverse problems. In this work the framework will be demonstrated on inverse aerodynamic design of 2D airfoil of turbine blades. inverse design invertible neural network machine...
Proc. ASME. GT2020, Volume 2C: Turbomachinery, V02CT35A003, September 21–25, 2020
Paper No: GT2020-14360
... recognize and eliminate the infeasible swirl distribution, and adjust the unsatisfactory swirl distribution using 2rC r . Proper blade shape and good impeller performance can be achieved with the help of the judgement criterion 2rC r . Keywords: centrifugal impeller; aerodynamic design; swirl...
Proc. ASME. GT2003, Volume 6: Turbo Expo 2003, Parts A and B, 1169-1173, June 16–19, 2003
Paper No: GT2003-38736
... of the flow solver regarding to the experimental tests. Using CFD in the aerodynamic design is a new area of research that can be a useful addition in this field. Aerodynamic design of a subsonic and transonic converged-diverged nozzle is the task of this work. ARC1D is a robust algorithm used...
Proc. ASME. GT2005, Volume 1: Turbo Expo 2005, 11-16, June 6–9, 2005
Paper No: GT2005-68045
... of the shafts and disks completely from the engine center, and places the attachment of the rotor blades in spanwise compression to a rotating casing. The preliminary aerodynamic design of the fan rotor blade estimated an overall adiabatic efficiency of 91.8%. The flow is supersonic near the blade leading edge...