Cold-flow Performance of Several Variations of a Ram-air-cooled Plug Nozzle for Supersonic-cruise Aircraft PDF Download
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Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
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Author: Douglas E. Harrington
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 44
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Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 116
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992
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Author: Oak Ridge National Laboratory
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 1458
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 2834
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
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Author: Stanley M. Nosek
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 29
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Book Description
Plug nozzle film cooling data were obtained downstream of a slot located at 42 percent of the total plug length on a J-85 engine. Film cooling reduced the aft end wall temperature as much as 150 K, reduced total pressure loss in the upstream convection cooling passages by 50 percent, and reduced estimated compressor bleed flow requirement by 14 percent compared to an all convectively cooled nozzle. Shock waves along the plug surface strongly influenced temperature distributions on both convection and film cooled portions. The effect was most severe at nozzle pressure ratios below 10 where adverse pressure gradients were most severe.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 586
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
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