A Theoretical and Experimental Investigation of Exhaust Ejectors for Cooling at Low Speeds PDF Download
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Author: R.E. Marquardt
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
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Author: R.E. Marquardt
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
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Author: C.F.E. Regnier
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Category :
Languages : en
Pages :
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Author:
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Category : Aerodynamics
Languages : en
Pages : 46
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Author: Frank L. Schwartz
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
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Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 388
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 836
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Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Author:
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Category : Aeronautics
Languages : en
Pages : 46
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Author:
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Category : Aeronautics
Languages : en
Pages : 664
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Author: Eugene J. Manganiello
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Category : Jet engines
Languages : en
Pages : 19
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An experimental investigation of rectangular exhaust-gas ejector pumps was conducted to provide data that would serve as a guide to the design of ejector applications for aircraft engines with marginal cooling. The pumping characteristics of rectangular ejectors actuated by the exhaust of a single-cylinder aircraft engine were determined for a range of mixing-section area from 20 to 50 square inches, over-all length from 12 to 42 inches, aspect ration from 1 to 5, diffusing exit area from 20 to 81 square inches, and aspect ratio of exhaust nozzle from 1 to 42. A few tests were conducted with a multistage ejector, a divided ejector, and an ejector incorporating bends along its length.
Author: J. Seddon
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 60
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