Author: H. J. Weigl
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2 - Jun 5, 1997.
Active stabilization of rotating stall and surge in a transonic single stage axial compressor, ASME 97-GT-411
Author: H. J. Weigl
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2 - Jun 5, 1997.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Orlando, FL, Jun 2 - Jun 5, 1997.
Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor
Author: Harald Jürgen Weigl
Publisher:
ISBN:
Category :
Languages : en
Pages : 302
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 302
Book Description
ASME Technical Papers
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 436
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 436
Book Description
An Investigation of Surge in a High-Speed Centrifugal Compressor Using Digital PIV
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Unsteady transition characteristics of rotating stall in a single-stage transonic axial compressor, ASME 99-GT-432
Author: Chaoqun Nie
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, Jun 7-Jun 10, 1999.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, Jun 7-Jun 10, 1999.
Paper
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 454
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 454
Book Description
35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 500
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 500
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 662
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 662
Book Description
Active Stabilization of Aeromechanical Systems
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 223
Book Description
This report details the work on the active control of surge and stall in gas turbine engines. The use of small amplitude waves predicted by theory as stall precursors were tested with experimental data. The nonlinear behavior of such waves was shown to explain much of the data in the literature. This theory was used to design an active stabilization system for rotating stall which was tested on both a single-stage and a three-stage axial compressor, increasing the stable operating range of the single-stage compressor by 25%. The dynamics of the three-stage compressor were shown to match closely with theory. The open- loop forced response characteristics of the compressors were measured and methodology developed in which this data was used to design the compressor control system. The models then developed were used to evaluate alternate control strategies. Engineering of the structural dynamics of the compression system was also shown to be successful in damping rotating stall and surge ... Active control, Compression system flow instabilities, Unsteady flow, Fluid-Structure interaction.
Publisher:
ISBN:
Category :
Languages : en
Pages : 223
Book Description
This report details the work on the active control of surge and stall in gas turbine engines. The use of small amplitude waves predicted by theory as stall precursors were tested with experimental data. The nonlinear behavior of such waves was shown to explain much of the data in the literature. This theory was used to design an active stabilization system for rotating stall which was tested on both a single-stage and a three-stage axial compressor, increasing the stable operating range of the single-stage compressor by 25%. The dynamics of the three-stage compressor were shown to match closely with theory. The open- loop forced response characteristics of the compressors were measured and methodology developed in which this data was used to design the compressor control system. The models then developed were used to evaluate alternate control strategies. Engineering of the structural dynamics of the compression system was also shown to be successful in damping rotating stall and surge ... Active control, Compression system flow instabilities, Unsteady flow, Fluid-Structure interaction.
21st AIAA Advanced Measurement and Ground Testing Technology Conference: 00-2201 - 00-2374
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 522
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 522
Book Description