Cold-air Performance of a Tip Turbine Designed to Drive a Lift Fan PDF Download
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Author:
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 25
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Author:
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 25
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Author:
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 23
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723252204
Category :
Languages : en
Pages : 28
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Book Description
Partial admission performance was obtained for a 0.4 linear scale version of the LF460 lift fan turbine over a range of speed from 40 to 140 percent of design equivalent speed and a range of scroll inlet total to diffuser exit static pressure ratio from 2.2 to 5.0. The investigation was conducted in two parts, with each part using a different side of the turbine scroll to simulate loss of a gas generator. Each side had an arc of admission of 180. Results are presented in terms of specific work, torque, mass flow, and efficiency. Haas, J. E. and Kofskey, M. G. and Hotz, G. M. and Futral, S. M., Jr. Glenn Research Center NASA-TM-X-3481, E-8914 RTOP 505-05
Author: Jeffery E. Hass
Publisher:
ISBN:
Category : Lift fans
Languages : en
Pages : 28
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Author: Jeffrey E. Haas
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Book Description
Author: Jeffery E. Hass
Publisher:
ISBN:
Category : Lift fans
Languages : en
Pages : 28
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Author:
Publisher:
ISBN:
Category : Lift fans
Languages : en
Pages : 36
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Author:
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ISBN:
Category : Astronautics
Languages : en
Pages : 532
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Author:
Publisher:
ISBN:
Category : Public administration
Languages : en
Pages : 1228
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