Treffer 1 - 14 von 14 für Suche 'Rebeske, John J', Suchdauer: 0,59s Treffer weiter einschränken
  1. 1
    Investigation of a NACA High-speed Optical Torquemeter

    Investigation of a NACA High-speed Optical Torquemeter von Rebeske, John J, Jr

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  2. 2
    Investigation of a NACA High-speed Strain-gage Torquemeter

    Investigation of a NACA High-speed Strain-gage Torquemeter von Rebeske, John J, Jr

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  3. 3
    Component Performance Investigation of J71 Experimental Turbine

    Component Performance Investigation of J71 Experimental Turbine von Rebeske, John J., Jr, Petrash, Donald A.

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  4. 4
    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics III : effect of turbine stator adjustment

    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics III : effect of turbine stator adjustment von Rohlik, Harold E, Rebeske, John J

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  5. 5
    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics I : effect of air bleed at compressor outlet

    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics I : effect of air bleed at compressor outlet von Rebeske, John J, Jr, Rohlik, Harold E

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  6. 6
    Investigation of losses in the XJ35-A-23 two-stage turbine

    Investigation of losses in the XJ35-A-23 two-stage turbine von Rebeske, John J, Jr, Forrette, Robert E

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  7. 7
    CONTOURED ENDWALL TURBINE STATOR

    CONTOURED ENDWALL TURBINE STATOR von BOOTH, THOMAS C, REBESKE, JOHN J, SWITZER, JACK R

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  8. 8
    Performance Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine II : Over-all Performance at Inlet Conditions of 35 Inches of Mercury Absolute and 700 Degree R

    Performance Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine II : Over-all Performance at Inlet Conditions of 35 Inches of Mercury Absolute and 700 Deg... von Forrette, Robert E, Schum, Harold J, Rebeske, John J, Jr

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  9. 9
    Investigation of Centrifugal Compressor Operated as a Centripetal Refrigeration Turbine

    Investigation of Centrifugal Compressor Operated as a Centripetal Refrigeration Turbine von Rebeske, John J, Jr, Parisen, Richard B, Schum, Harold J

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  10. 10
    Performance Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine : Over-all Performance with Standard Rotor Blading at Inlet Conditions of 35 Inches of Mercury Absolute and 700 R

    Performance Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine : Over-all Performance with Standard Rotor Blading at Inlet Conditions of 35 Inches of Mer... von Berkey, William E, Rebeske, John J, Jr, Forrette, Robert E

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  11. 11
    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed

    Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed von Rebeske, John J, Jr, Dugan, James F, Jr

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  12. 12
    Matched Performance Characteristics of a 16-stage Axial-flow Compressor and a 3-stage Turbine

    Matched Performance Characteristics of a 16-stage Axial-flow Compressor and a 3-stage Turbine von Rebeske, John J, Jr, Dugan, James F, Jr

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  13. 13
    Over-all Performance of J35-A-23 Two-stage Turbine

    Over-all Performance of J35-A-23 Two-stage Turbine von Rebeske, John J, Jr, Berkey, William E, Forrette, Robert E

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  14. 14
    Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine

    Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine von Dugan, James F., Jr, Rebeske, John J., Jr, Finger, Harold B.

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