HP Vane Aerodynamics and Heat Transfer in the Presence of Aggressive Inlet Swirl

HP Vane Aerodynamics and Heat Transfer in the Presence of Aggressive Inlet Swirl

Показать другие версии (1)

Modern lean burn combustors now employ aggressive swirlers to enhance fuel-air mixing and improve flame stability. The flow at combustor exit can therefore have high residual swirl. A good deal of research concerning the flow within the combustor is available in open literature. The impact of swirl...

Полное описание

Библиографические подробности
Главные авторы:	Qureshi, I, Smith, A, Povey, T
Формат:	Journal article
Язык:	English
Опубликовано:	2013

Схожие документы

HP VANE AERODYNAMICS AND HEAT TRANSFER IN THE PRESENCE OF AGGRESSIVE INLET SWIRL
по: Qureshi, I, и др.
Опубликовано: (2012)

EFFECT OF AGGRESSIVE INLET SWIRL ON HEAT TRANSFER AND AERODYNAMICS IN AN UNSHROUDED TRANSONIC HP TURBINE
по: Qureshi, I, и др.
Опубликовано: (2012)

Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine
по: Qureshi, I, и др.
Опубликовано: (2012)

Heat transfer and aerodynamics of an intermediate pressure nozzle guide vane with and without inlet temperature non-uniformity
по: Chana, K, и др.
Опубликовано: (2003)

EFFECT OF STIMULATED COMBUSTOR TEMPERATURE NONUNIFORMITY ON HP VANE AND ENDWALL HEAT TRANSFER: AN EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION
по: Qureshi, I, и др.
Опубликовано: (2010)

Effect of Simulated Combustor Temperature Nonuniformity on HP Vane and End Wall Heat Transfer: An Experimental and Computational Investigation
по: Qureshi, I, и др.
Опубликовано: (2011)

The effect of hot-streaks on HP vane surface and endwall heat transfer: An experimental and numerical study
по: Povey, T, и др.
Опубликовано: (2007)

The effect of hot-streaks on HP vane surface and endwall heat transfer: An experimental and numerical study
по: Povey, T, и др.
Опубликовано: (2005)

Effect of Temperature Nonuniformity on Heat Transfer in an Unshrouded Transonic HP Turbine: An Experimental and Computational Investigation
по: Qureshi, I, и др.
Опубликовано: (2012)

Effects of Inlet Swirl Distortion on a Multi-Stage Compressor with Inlet Guide Vanes and Stall Margin Enhancement Method
по: Yibo Fang, и др.
Опубликовано: (2023-02-01)

Effect of low-NO X combustor swirl clocking on intermediate turbine duct vane aerodynamics with an upstream high pressure turbine stage — An experimental and computational study
по: Johansson, M, и др.
Опубликовано: (2016)

Aerodynamic design of moveable inlet guide vanes for active control of rotating stall
по: Silkowski, Peter D. (Peter Daniel)
Опубликовано: (2008)

EFFECT OF TEMPERATURE NONUNIFORMITY ON HEAT TRANSFER IN AN UNSHROUDED TRANSONIC HP TURBINE: AN EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION
по: Qureshi, I, и др.
Опубликовано: (2010)

Experimental and Computational Study on Effect of Vanes on Heat Transfer and Flow Structure of Swirling Impinging Jet
по: S. M. Illyas, и др.
Опубликовано: (2022-11-01)

Aerodynamic design schemes of the inlet guide vane in a core-driven fan stage
по: Hui Cao, и др.
Опубликовано: (2018-01-01)

Heat transfer measurements on an intermediate-pressure nozzle guide vane tested in a rotating annular turbine facility, and the modifying effects of a non-uniform inlet temperature profile
по: Povey, T, и др.
Опубликовано: (2003)

Impact of Slots on the Aerodynamic Performance of the Variable Inlet Guide Vane Cascade of a Centrifugal Compressor
по: J. Xin, и др.
Опубликовано: (2022-11-01)

Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane
по: Haifen Du, и др.
Опубликовано: (2019-10-01)

Aerodynamic and thermal field development of cooled transonic HP NGV
по: Amend, J, и др.
Опубликовано: (2023)

Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages
по: Simone, S, и др.
Опубликовано: (2012)

Effects of Feeding Mode and Inlet Area Ratio on Heating Characteristics in Dual-Inlet Swirl Tubes
по: X. Xu, и др.
Опубликовано: (2021-01-01)

Effect of the Reynolds Number and Clearance Flow on the Aerodynamic Characteristics of a New Variable Inlet Guide Vane
по: Hengtao Shi
Опубликовано: (2021-06-01)

ANALYSIS ON THE EFFECT OF A NON-UNIFORM INLET PROFILE ON HEAT TRANSFER AND FLUID FLOW IN TURBINE STAGES
по: Simone, S, и др.
Опубликовано: (2010)

Swirl Flow and Heat Transfer in a Rotor-Stator Cavity with Consideration of the Inlet Seal Thermal Deformation Effect
по: Yu Shi, и др.
Опубликовано: (2023-01-01)

A combustor-representative swirl simulator for a transonic turbine research facility
по: Qureshi, I, и др.
Опубликовано: (2011)

Experimental study of impact of in-service deterioration on aerodynamic performance of high-pressure nozzle guide vanes
по: Michaud, M, и др.
Опубликовано: (2023)

Design optimization of a vane type pre-swirl nozzle
по: Jungsoo Lee, и др.
Опубликовано: (2021-01-01)

Investigation of the Flow Field and Aerodynamic Load on Impellers under Guide Vanes with a Self-Induced Slot in Compressor Radial Inlet
по: Jianchi Xin, и др.
Опубликовано: (2022-05-01)

Numerical investigation of variable inlet guide vanes with trailing-edge dual slots to decrease the aerodynamic load on centrifugal compressor impeller
по: Jianchi Xin, и др.
Опубликовано: (2016-03-01)

Aerodynamics of a swirling fluidized bed
по: Mohd Nawi, Mohd Al-Hafiz
Опубликовано: (2013)

Swirling Flow Prediction in Model Combustor with Axial Guide Vane Swirler
по: J. Vondál, и др.
Опубликовано: (2012-09-01)

Loss Characterization of a Conventional Variable Inlet Guide Vane
по: Roman G. Frank, и др.
Опубликовано: (2021-07-01)

Role of flow alignment and inlet blockage on vaned diffuser performance
по: Phillips, Michael Stephen
Опубликовано: (2016)

Effects of inlet air holes on swirl flow characteristics and outlet temperature distribution in an axial swirl combustor
по: Yanzhao An, и др.
Опубликовано: (2024-09-01)

Effect of various inlet geometries on swirling flow in can combustor
по: W. Treedet, и др.
Опубликовано: (2018-06-01)

Simulation study on the effect of fuel-inlet angle on the swirling combustion /
по: Ng, Wing Chun, 1991- , author 610960, и др.
Опубликовано: (2017)

Simulation study on the effect of fuel-inlet angle on the swirling combustion /
по: Ng, Wing Chun, 1991-, author 610960
Опубликовано: (2017)

Turbine heat transfer and aerodynamic measurements and predictions for A 1.5 Stage configuration
по: Chana, K, и др.
Опубликовано: (2004)

Improvement in energy performance from the construction of inlet guide vane and diffuser vane geometries in an axial-flow pump
по: Duc-Anh Nguyen, и др.
Опубликовано: (2024-01-01)

Investigation of Unsteady Flow Phenomena in First Vane Caused by Combustor Flow With Swirl
по: Jacobi, S, и др.
Опубликовано: (2017)