Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Presented at the International Gas Turbine and Aeroengine Congress &Exhibition Birmingham, UK - June 10-13, 1996.
An Experimental Determination of Losses in a 3-Port Wave Rotor
Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Presented at the International Gas Turbine and Aeroengine Congress &Exhibition Birmingham, UK - June 10-13, 1996.
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Presented at the International Gas Turbine and Aeroengine Congress &Exhibition Birmingham, UK - June 10-13, 1996.
An Experiment on Losses in a Three-Port Wave Rotor
Wave-Rotor-Enhanced Gas Turbine Engine Demonstrator
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
The U.S. Army Research Laboratory, NASA Glenn Research Center, and Rolls-Royce Allison are working collaboratively to demonstrate the benefits and viability of a wave-rotor-topped gas turbine engine. The self-cooled wave rotor is predicted to increase the engine overall pressure ratio and peak temperature by 300% and 25 to 30%, respectively, providing substantial improvements in engine efficiency and specific power. Such performance improvements would significantly reduce engine emissions and the fuel logistics trails of armed forces. Progress towards a planned demonstration of a wave-rotor-topped Rolls-Royce Allison model 250 engine has included completion of the preliminary design and layout of the engine, the aerodynamic design of the wave rotor component and prediction of its aerodynamic performance characteristics in on- and off-design operation and during transients, and the aerodynamic design of transition ducts between the wave rotor and the high pressure turbine. The topping cycle increases the burner entry temperature and poses a design challenge to be met in the development of the demonstrator engine.
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
The U.S. Army Research Laboratory, NASA Glenn Research Center, and Rolls-Royce Allison are working collaboratively to demonstrate the benefits and viability of a wave-rotor-topped gas turbine engine. The self-cooled wave rotor is predicted to increase the engine overall pressure ratio and peak temperature by 300% and 25 to 30%, respectively, providing substantial improvements in engine efficiency and specific power. Such performance improvements would significantly reduce engine emissions and the fuel logistics trails of armed forces. Progress towards a planned demonstration of a wave-rotor-topped Rolls-Royce Allison model 250 engine has included completion of the preliminary design and layout of the engine, the aerodynamic design of the wave rotor component and prediction of its aerodynamic performance characteristics in on- and off-design operation and during transients, and the aerodynamic design of transition ducts between the wave rotor and the high pressure turbine. The topping cycle increases the burner entry temperature and poses a design challenge to be met in the development of the demonstrator engine.
Scientific and Technical Aerospace Reports
NASA Technical Memorandum
ASME Technical Papers
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 596
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 596
Book Description
An Incidence Loss Model for Wave Rotors with Axially Aligned Passages
Author: Daniel E. Paxson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 16
Book Description
Design of the NASA Lewis 4-Port Wave Rotor Experiment
Proceedings of the ASME Process Industries Division, ... : Presented at the ... ASME Mechanical Engineering Congress and Exposition, ...
Paper
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 598
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 598
Book Description