An Experimental Determination of Losses in a 3-Port Wave Rotor PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download An Experimental Determination of Losses in a 3-Port Wave Rotor PDF full book. Access full book title An Experimental Determination of Losses in a 3-Port Wave Rotor by Jack Wilson. Download full books in PDF and EPUB format.

An Experimental Determination of Losses in a 3-Port Wave Rotor

An Experimental Determination of Losses in a 3-Port Wave Rotor PDF 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

An Experimental Determination of Losses in a 3-Port Wave Rotor PDF 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 Experiment on Losses in a Three-Port Wave Rotor

An Experiment on Losses in a Three-Port Wave Rotor PDF Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Wave-Rotor-Enhanced Gas Turbine Engine Demonstrator

Wave-Rotor-Enhanced Gas Turbine Engine Demonstrator PDF 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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 492

Book Description


ASME Technical Papers

ASME Technical Papers PDF Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 596

Book Description


An Incidence Loss Model for Wave Rotors with Axially Aligned Passages

An Incidence Loss Model for Wave Rotors with Axially Aligned Passages PDF Author: Daniel E. Paxson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 16

Book Description


Design of the NASA Lewis 4-Port Wave Rotor Experiment

Design of the NASA Lewis 4-Port Wave Rotor Experiment PDF Author: Jack Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 12

Book Description


Proceedings of the ASME Process Industries Division, ... : Presented at the ... ASME Mechanical Engineering Congress and Exposition, ...

Proceedings of the ASME Process Industries Division, ... : Presented at the ... ASME Mechanical Engineering Congress and Exposition, ... PDF Author:
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 246

Book Description


Paper

Paper PDF Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 598

Book Description