Design of the NASA Lewis 4-Port Wave Rotor Experiment PDF Download
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Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
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Book Description
Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Get Book Here
Book Description
Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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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.
Author:
Publisher: DIANE Publishing
ISBN: 1428918256
Category :
Languages : en
Pages : 190
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Author:
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ISBN:
Category : Airplanes
Languages : en
Pages : 662
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 626
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![Integration of a Wave Rotor to an Ultra-micro Gas Turbine (U[mu]GT) PDF](https://books.google.com/books/content/images/frontcover/RQVM8uAEfc4C?fife=w80-h100)
Author: Florin Iancu
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 566
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Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1932
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Author:
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 246
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Author:
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 488
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