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  1. 1
    A technique applicable to the aerodynamic design of inducer-type multistage axial-flow compressors /

    A technique applicable to the aerodynamic design of inducer-type multistage axial-flow compressors / by Savage, Melvyn

    Published 1952
    Government Document Book
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  2. 2
    Analysis of an axial compressor stage with infinitesimal and finite blade spacing /

    Analysis of an axial compressor stage with infinitesimal and finite blade spacing / by Reissner, Hans J. (Hans Jacob), 1874-1967

    Published 1951
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  3. 3
    An analytical investigation using aerodynamic limitations of several designs of high stage pressure ratio multistage compressors /

    An analytical investigation using aerodynamic limitations of several designs of high stage pressure ratio multistage compressors / by Voit, Charles H.

    Published 1951
    Government Document Book
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  4. 4
    Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors /

    Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors / by Wu, Chung-Hua

    Published 1950
    Government Document Book
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  5. 5
    Method of experimentally determining radial distributions of velocity through axial-flow compressor /

    Method of experimentally determining radial distributions of velocity through axial-flow compressor / by Finger, Harold B.

    Published 1950
    Government Document Book
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  6. 6
    Investigation of rotating stall in a single-stage axial compressor /

    Investigation of rotating stall in a single-stage axial compressor / by Montgomery, Stephen R.

    Published 1957
    Government Document Book
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  7. 7
    Compressor instability with integral methods

    Compressor instability with integral methods by Ng, Y. K. Eddie

    Published 2007
    Full Text (via Springer)
    Electronic eBook
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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
    NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results /

    NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results / by Schulze, Wallace M.

    Published 1957
    Government Document Book
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  10. 10
    Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests /

    Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests / by Godwin, William R.

    Published 1957
    Government Document Book
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  11. 11
    Recent results on high-pressure axial blowers /

    Recent results on high-pressure axial blowers / by Eckert, B. (Bruno), 1907-

    Published 1947
    Government Document Book
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  12. 12
    The influence of the diameter ratio on the characteristics diagram of the axial compressor /

    The influence of the diameter ratio on the characteristics diagram of the axial compressor / by Eckert, B. (Bruno), 1907-

    Published 1948
    Government Document Book
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  13. 13
    Determination of surge and stall limits of an axial-flow turbojet engine for control applications /

    Determination of surge and stall limits of an axial-flow turbojet engine for control applications / by Schmidt, Ross D.

    Published 1957
    Government Document Book
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  14. 14
    Performance at low speeds of compressor rotors having low-cambered NACA 65-series blades with high inlet angles and low solidities /

    Performance at low speeds of compressor rotors having low-cambered NACA 65-series blades with high inlet angles and low solidities / by Emery, James C.

    Published 1958
    Government Document Book
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  15. 15
    Experimental investigation of cermet turbine blades in an axial-flow turbojet engine /

    Experimental investigation of cermet turbine blades in an axial-flow turbojet engine / by Morgan, William C.

    Published 1957
    Government Document Book
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  16. 16
    Alternating pressures and blade stresses in an axial-flow compressor /

    Alternating pressures and blade stresses in an axial-flow compressor / by Forshaw, J. R.

    Published 1956
    Book
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  17. 17
    Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed /

    Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed / by Westphal, Willard R.

    Published 1958
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  18. 18
    Axial-flow compressors : a strategy for aerodynamic design and analysis /

    Axial-flow compressors : a strategy for aerodynamic design and analysis / by Aungier, Ronald H.

    Published 2003
    Book
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  19. 19
    Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory /

    Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory / by Sinnette, John T.

    Published 1944
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  20. 20
    Performance of NACA eight-stage axial-flow compressor at simulated altitude /

    Performance of NACA eight-stage axial-flow compressor at simulated altitude / by King, J. Austin

    Published 1944
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