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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Author: A. Kahane
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 578
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Book Description
Charts are presented to show the pressure rise that is obtainable in an engine-cooling installation with a typical airfoil-type propeller-speed fan. The charts cover fans of the stator-rotor, rotor-stator, and rotor alone configurations, with blades incorporating both the highly cambered 65-series blower-blade sections and the conventional low-cambered airfoil sections. The effects of operation of a geared fan with rotational speeds limited by compressibility considerations and the effects of initial rotational inflow are indicated. Use of the charts to predict the pressure rise obtainable with any fan of the types considered is illustrated in a sample calculation.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 434
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 462
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1620
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1540
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author: Paul F. Borchers
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 134
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 544
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In order to establish a standard procedure for rating and testing multistage axial-flow compressors, the NACA Subcommittee on Compressors appointed a panel to write such a procedure. This panel made recommendations for standardization of test setups, instrumentation, test procedure, data to be taken, and the presentation of the data. These recommendations are presented.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 130
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