Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Design of the NASA Lewis 4-Port Wave Rotor Experiment
Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Initial Results from the NASA-Lewis Wave Rotor Experiment
Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Book Description
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.
Research & Technology 1997
Author:
Publisher: DIANE Publishing
ISBN: 1428918256
Category :
Languages : en
Pages : 190
Book Description
Publisher: DIANE Publishing
ISBN: 1428918256
Category :
Languages : en
Pages : 190
Book Description
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 662
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 662
Book Description
33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 626
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 626
Book Description
Integration of a Wave Rotor to an Ultra-micro Gas Turbine (U[mu]GT)
Author: Florin Iancu
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 566
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 566
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1932
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1932
Book Description
Proceedings of the ASME Process Industries Division, ... : Presented at the ... ASME Mechanical Engineering Congress and Exposition, ...
Author:
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 246
Book Description
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 246
Book Description
Journal of Engineering for Gas Turbines and Power
Author:
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 488
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 488
Book Description