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Analysis Of Supersonic Plug Nozzle Flowfield And Heat Transfer
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722944605 Total Pages :180 pages Book Rating :4.9/5 (446 download)
Book Synopsis Analysis of Supersonic Plug Nozzle Flowfield and Heat Transfer by : National Aeronautics and Space Administration (NASA)
Download or read book Analysis of Supersonic Plug Nozzle Flowfield and Heat Transfer written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt: A number of problems pertaining to the flowfield in a plug nozzle, designed as a supersonic thruster nozzle, with provision for cooling the plug with a coolant stream admitted parallel to the plug wall surface, were studied. First, an analysis was performed of the inviscid, nonturbulent, gas dynamic interaction between the primary hot stream and the secondary coolant stream. A numerical prediction code for establishing the resulting flowfield with a dividing surface between the two streams, for various combinations of stagnation and static properties of the two streams, was utilized for illustrating the nature of interactions. Secondly, skin friction coefficient, heat transfer coefficient and heat flux to the plug wall were analyzed under smooth flow conditions (without shocks or separation) for various coolant flow conditions. A numerical code was suitably modified and utilized for the determination of heat transfer parameters in a number of cases for which data are available. Thirdly, an analysis was initiated for modeling turbulence processes in transonic shock-boundary layer interaction without the appearance of flow separation. Murthy, S. N. B. and Sheu, W. H. Unspecified Center BOUNDARY LAYER FLOW; FLOW DISTRIBUTION; HEAT TRANSFER; PLUG NOZZLES; SUPERSONIC NOZZLES; SURFACE COOLING; HEAT FLUX; INTERACTIONAL AERODYNAMICS; REYNOLDS STRESS; SHOCK LAYERS; SKIN FRICTION; STAGNATION POINT; VORTICES...
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