˜Aœ study of the flow field produced by an axisymmetric underexpanded jet exhausting into a cylindrical tube PDF Download
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Author: James Lucian Batson
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ISBN:
Category :
Languages : en
Pages : 106
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Author: James Lucian Batson
Publisher:
ISBN:
Category :
Languages : en
Pages : 106
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Author: James Lucian Batson
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Category : Jet propulsion
Languages : en
Pages : 212
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Author:
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Category : Aeronautics
Languages : en
Pages : 1460
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: John J. Bertin
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Category :
Languages : en
Pages : 112
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An underexpanded, supersonic jet of cold nitrogen was exhausted into a constrictive, stepped launch tube. For one launch tube, the reduction in cross section was accomplished abruptly by a rectangular step. For the other launch tube, the reduction in cross section was accomplished gradually by a 15 degree-ramp. Thirty-seven static-pressure orifices were located along the walls of the two tubes. By varying the location of the nozzle exit-plane with respect to the step location, one could simulate (in a quasi-steady manner) the effect of movement of the rocket through the launch tube. Pitot probes located in the annular region between the simulated rocket-nozzle and the launch tube provided information about the reverse, or blow-by, flow created when the nozzle exhaust encountered the constriction. (Modified author abstract).
Author:
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Category : Mechanics, Applied
Languages : en
Pages : 520
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Category : Dissertations, Academic
Languages : en
Pages : 914
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Author:
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Category :
Languages : en
Pages : 746
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 594
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Author:
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Category : Science
Languages : en
Pages : 828
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Author:
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Category : Dissertation abstracts
Languages : en
Pages : 642
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