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An Experimental Determination Of Losses In A 3 Port Wave Rotor

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An Experimental Determination Of Losses In A 3 Port Wave Rotor

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Author : Jack Wilson
language : en
Publisher:
Release Date : 1996

An Experimental Determination Of Losses In A 3 Port Wave Rotor written by Jack Wilson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.

Presented at the International Gas Turbine and Aeroengine Congress &Exhibition Birmingham, UK - June 10-13, 1996.

Design Of The Nasa Lewis 4 Port Wave Rotor Experiment

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Author : Jack Wilson
language : en
Publisher:
Release Date : 1997

Design Of The Nasa Lewis 4 Port Wave Rotor Experiment written by Jack Wilson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with categories.

Wave Rotor Enhanced Gas Turbine Engine Demonstrator

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Author :
language : en
Publisher:
Release Date : 1999

Wave Rotor Enhanced Gas Turbine Engine Demonstrator written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.

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.

An Incidence Loss Model For Wave Rotors With Axially Aligned Passages

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Author : Daniel E. Paxson
language : en
Publisher:
Release Date : 1998

An Incidence Loss Model For Wave Rotors With Axially Aligned Passages written by Daniel E. Paxson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics categories.