1–20 von 22 Ergebnissen
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    Theory and tunnel tests of rotor blades for supersonic turbines

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

    The industrial gas turbine

    Roberson, E. C. | SLUB | 1951

    The design and testing of an axial compressor having a mean stage temperature rise of 30 deg C

    Carter, A. D. S. / Andrews, S. J. / Fielder, E. A. | SLUB | 1957

    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

    Blade vibratory stresses in a multi-stage axial flow compressor

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

    An experimental investigation of a thick aerofoil nozzle cascade

    Andrews, S. J. / Schofield, N. W. | SLUB | 1956

    A method of performance estimation for axial flow turbines

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

    Alternating pressures and blade stresses in an axial flow compressor

    Forshaw, J. R. / Taylor, H. / Chaplin, R. | SLUB | 1956