1–20 von 74 Ergebnissen
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    Technology innovation and exploitation : innovative technologies for future gas-turbine core-engines

    Freier Zugriff
    Rolls-Royce Deutschland Ltd & Co KG | TIBKAT | 2017

    Impingement jet cooling in gas turbines

    Amano, Ryoichi S. / Sundén, Bengt | TIBKAT | 2014

    Theory and tunnel tests of rotor blades for supersonic turbines

    Stratford, B. S. / Sansome, G. E. | SLUB | 1962

    Tests concerning novel designs of blades for axial compressors

    Andrews, S. J. / Jeffs, R. A. / Hartley, E. L. | TIBKAT | 1956

    A method of performance estimation for axial flow turbines

    Ainley, D. G. / Mathieson, G. C. R. | TIBKAT | 1957

    Blade vibratory stresses in a multi-stage axial flow compressor

    Kilpatrick, D. A. / Carter, A. D. S. / O'Neill, L. | SLUB | 1961

    The component pressure losses in combustion chambers

    Knight, H. A. / Walker, Robin B. | SLUB | 1957

    Tests concerning novel designs of blades for axial compressors

    Andrews, S. J. / Jeffs, R. A. / Hartley, E. L. | SLUB | 1956