Application of a three-dimensional viscous transonic inverse method to NASA rotor 67 [PDF]
, 2002 The development and application of a three-dimensional inverse methodology in which the blade geometry is computed on the basis of the specification of static pressure loading distribution is presented.
Tiow, W.T., Zangeneh, M.
core +1 more source
Experimental study of transonic flow over a wind turbine airfoil [PDF]
Wind Energy ScienceFor the largest wind turbines currently being designed, operation close to cut-out conditions can lead to the tip airfoil experiencing transonic flow conditions.
A. Aditya +5 more
doaj +1 more source
Structural and Aerodynamical Parametric Study of Truss-Core Gas Turbine Rotor Blade [PDF]
Journal of Applied and Computational Mechanics, 2021 Improvement of turbine blades is currently the prime area of research dedicated to the development of more efficient gas turbines. This study examines the structural performance of the gas turbine rotor and stator blades with the implementation of Kagome
Dulat Akzhigitov +3 more
doaj +1 more source
Causes and Solution of Aperiodicity of Supersonic Flow Field Downstream of a Profile Cascade
Communications, 2012 The paper deals with problems of transonic flow field periodicity downstream of a profile cascade with finite number of blades. The origin of phenomena generating this aperiodicity in transonic wind tunnel is described.
Martin Luxa +3 more
doaj +1 more source
Numerical analysis of transonic flow over the FFA-W3-211 wind turbine tip airfoil [PDF]
Wind Energy ScienceModern wind turbines are the largest rotating machines ever built, with blade lengths exceeding 100 m. Previous studies demonstrated how the flow around the tip airfoils of such large machines reaches local flow Mach numbers (Ma), at which the ...
M. C. Vitulano +4 more
doaj +1 more source
NUMERICAL SIMULATION OF THE LAMINAR-TURBULENT TRANSITION IN A HIGH-LOADED TRANSONIC TURBINE CASCADE
Авіаційно-космічна техніка та технологія, 2017 A three-dimensional turbulent flow of a viscous compressible gas through a high-loaded transonic turbine cascade is considered, taking into account the laminar-turbulent transition.
С. В. Ершов +2 more
doaj +1 more source
Focusing Schlieren Visualization of Transonic Turbine Tip-Leakage Flows
International Journal of Turbomachinery, Propulsion and Power, 2020 This paper presents a focusing schlieren system designed for the investigation of transonic turbine tip-leakage flows. In the first part, the functional principle and the design of the system are presented. Major design considerations and necessary trade-
Maximilian Passmann +2 more
doaj +1 more source
Aerodynamics and Sealing Performance of the Downstream Hub Rim Seal in a High-Pressure Turbine Stage
International Journal of Turbomachinery, Propulsion and Power, 2023 The purpose of the paper is to characterize the aerodynamic behavior of a rotor-downstream hub cavity rim seal in a high-pressure turbine (HPT) stage.
Filippo Merli +4 more
doaj +1 more source
Endwall aerodynamic losses from turbine components within gas turbine engines
Propulsion and Power Research, 2017 A survey of research on aerodynamic loss investigations for turbine components of gas turbine engines is presented. Experimental and numerically predicted results are presented from investigations undertaken over the past 65 plus years.
Phil Ligrani +2 more
doaj +1 more source
Encounters with Vortices in a Turbine Nozzle Passage
International Journal of Rotating Machinery, 2012 Experiments were conducted on the flow through a transonic turbine cascade. Secondary flows and a wide range of vortex types were encountered, including horseshoe vortices, shock-induced passage vortices, and streamwise vortices on the suction surface ...
J. P. Gostelow +3 more
doaj +1 more source