Numerical Analysis of Ignition Transient in an Axisymmetric Solid Rocket Motor Equipped with Rear Ignition System PDF Download
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Author: Seung-Wook Baek
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Category :
Languages : en
Pages :
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Author: Seung-Wook Baek
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Languages : en
Pages :
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Author: In-Hyun Cho
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Category :
Languages : en
Pages :
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Category : Mechanics, Applied
Languages : en
Pages : 742
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Category : Aeronautics
Languages : en
Pages : 1032
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Category : Airplanes
Languages : en
Pages : 576
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Author: Gary Daniel Luke
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Category : Internal combustion engines
Languages : en
Pages : 422
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Author: W. A. Johnston
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Category :
Languages : en
Pages :
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Author:
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Category : Aeronautics
Languages : en
Pages : 654
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722082550
Category :
Languages : en
Pages : 42
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This report presents the results obtained from an experimental analysis of the flow field in the slots of the star grain section in the head-end of the advanced solid rocket motor during the ignition transient. This work represents an extension of the previous tests and analysis to include the effects of using a center port in conjunction with multiple canted igniter ports. The flow field measurements include oil smear data on the star slot walls, pressure and heat transfer coefficient measurements on the star slot walls and velocity measurements in the star slot. Foster, Winfred A., Jr. and Jenkins, Rhonald M. Unspecified Center NAG8-923...
Author: Tae-Seong Roh
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Category :
Languages : en
Pages :
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