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Development And Validation Of A Supersonic Helium Air Coannular Jet Facility
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Book Synopsis Development and Validation of a Supersonic Helium-Air Coannular Jet Facility by : Atherton A. Carty
Download or read book Development and Validation of a Supersonic Helium-Air Coannular Jet Facility written by Atherton A. Carty and published by . This book was released on 1999 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data are acquired in a simple coannular He/air supersonic jet suitable for validation of CFD codes for high speed propulsion. Helium is employed as a non-reacting hydrogen fuel simulant, constituting the core of the coannular flow while the coflow is composed of air. The mixing layer interface between the two flows in the near field and the plume region which develops further downstream constitute the primary regions of interest, similar to those present in all hypersonic air breathing propulsion systems. A computational code has been implemented from the experiment's inception, serving as a tool for model design during the development phase.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721084333 Total Pages :112 pages Book Rating :4.0/5 (843 download)
Book Synopsis Development and Validation of a Supersonic Helium-Air Coannular Jet Facility by : National Aeronautics and Space Administration (NASA)
Download or read book Development and Validation of a Supersonic Helium-Air Coannular Jet Facility written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-13 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data are acquired in a simple coannular He/air supersonic jet suitable for validation of CFD (Computational Fluid Dynamics) codes for high speed propulsion. Helium is employed as a non-reacting hydrogen fuel simulant, constituting the core of the coannular flow while the coflow is composed of air. The mixing layer interface between the two flows in the near field and the plume region which develops further downstream constitute the primary regions of interest, similar to those present in all hypersonic air breathing propulsion systems. A computational code has been implemented from the experiment's inception, serving as a tool for model design during the development phase. Carty, Atherton A. and Cutler, Andrew D. Langley Research Center NCC1-217; RTOP 522-51-31-10
Book Synopsis NASA Langley Scientific and Technical Information Output: 1999 by :
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Book Synopsis Advanced Turbulent Combustion Physics and Applications by : N. Swaminathan
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Book Synopsis 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-3850 - 02-3899 by :
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