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Title
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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control
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Date
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1953
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Index Abstract
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Coming Soon
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Photo Quality
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Undetermined
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Report Number
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WADC TR 52-128 Part 2
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Creator
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De Leo, Richard V.
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Corporate Author
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Rosemount Aeronautical Laboratories, University of Minnesota
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Laboratory
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Aircraft Laboratory
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Extent
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90
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NTRL Accession Number
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AD054379
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Identifier
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AD0054379
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Access Rights
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Unknown
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Distribution Classification
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1
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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AFAL ltr
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Distribution Change Action Date
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10/18/2001
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Abstract
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The primary purpose of Phase II of the ejector study has been to provide experimental data for engineering design purposes. The geometric and state parameters of the ejector were investigated over a wide range, both with and wfthaut diffuser. Variation in the ejector performance was determined for a change in primary temperature, and the effect of the use of a supersonic primary nozzle was also investigated. Comparisons of theoretical and experimental pumping performance without diffuser are presented.
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Report Availability
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Not available via Contrails
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Date Issued
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1953-12
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Index In
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U.S. Government Research Reports
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Type
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report