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  1. 1
    Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams /

    Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams / by Ingebo, Robert D.

    Published 1981
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  2. 2
    Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes /

    Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes / by Ellis, Gaylord O.

    Published 1951
    Government Document Book
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  3. 3
    Linearized supersonic axially symmetric flow about open-nosed bodies obtained by use of stream function /

    Linearized supersonic axially symmetric flow about open-nosed bodies obtained by use of stream function / by Moore, F. K. (Franklin K.)

    Published 1950
    Government Document Book
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  4. 4
    An analysis of base pressure at supersonic velocities and comparison with experiment /

    An analysis of base pressure at supersonic velocities and comparison with experiment / by Chapman, Dean R.

    Published 1950
    Government Document Book
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  5. 5
    An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second /

    An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second / by Prian, Vasily D.

    Published 1951
    Government Document Book
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  6. 6
    Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines /

    Possible application of blade boundary-layer control to improvement of design and off-design performance of axial-flow turbomachines / by Sinnette, John T.

    Published 1951
    Government Document Book
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  7. 7
    Analytical investigation of some three-dimensional flow problems in turbomachines /

    Analytical investigation of some three-dimensional flow problems in turbomachines / by Marble, Frank E.

    Published 1952
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  8. 8
    Influence of wall boundary layer upon the performance of an axial-flow fan rotor /

    Influence of wall boundary layer upon the performance of an axial-flow fan rotor / by Boxer, Emanuel

    Published 1951
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  9. 9
    Axial-momentum theory for propellers in compressible flow /

    Axial-momentum theory for propellers in compressible flow / by Vogeley, A. W. (Arthur W.)

    Published 1951
    Government Document Book
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  10. 10
    Approximate design method for high-solidity blade elements in compressors and turbines /

    Approximate design method for high-solidity blade elements in compressors and turbines / by Stanitz, John D.

    Published 1951
    Government Document Book
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  11. 11
    Effect of heat and power extraction on turbojet-engine performance. : 2 - Effect of compressor-outlet air bleed for specific modes of engine operation /

    Effect of heat and power extraction on turbojet-engine performance. : 2 - Effect of compressor-outlet air bleed for specific modes of engine operation / by Rom, Frank E.

    Published 1950
    Government Document Book
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  12. 12
    Turning-angle design rules for constant-thickness circular-arc inlet guide vanes in axial annular flow /

    Turning-angle design rules for constant-thickness circular-arc inlet guide vanes in axial annular flow / by Lieblein, Seymour

    Published 1950
    Government Document Book
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  13. 13
    Compressibility correction for turning angles of axial-flow inlet guide vanes /

    Compressibility correction for turning angles of axial-flow inlet guide vanes / by Lieblein, Seymour

    Published 1950
    Government Document Book
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  14. 14
    The linearized characteristics method and its application to practical nonlinear supersonic problems /

    The linearized characteristics method and its application to practical nonlinear supersonic problems / by Ferri, Antonio, 1912-1975

    Published 1951
    Government Document Book
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  15. 15
    Minimum wave drag of bodies of revolution with a cylindrical center section /

    Minimum wave drag of bodies of revolution with a cylindrical center section / by Fuller, Franklyn B.

    Published 1951
    Government Document Book
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  16. 16
    An approximate solution for axially symmetric flow over a cone with an attached shock wave /

    An approximate solution for axially symmetric flow over a cone with an attached shock wave / by Hord, Richard A.

    Published 1955
    Government Document Book
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  17. 17
    Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section /

    Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section / by Evvard, John C.

    Published 1952
    Government Document Book
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  18. 18
    One-dimensional analysis of choked-flow turbines /

    One-dimensional analysis of choked-flow turbines / by English, Robert E. (Robert Eugene)

    Published 1952
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  19. 19
    A note on secondary flow in rotating radial channels /

    A note on secondary flow in rotating radial channels / by Kramer, James J.

    Published 1953
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  20. 20
    Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack /

    Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignm... by Stanitz, John D.

    Published 1953
    Government Document Book
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