Paper 19: Investigation of Supersonic Flow through the Tip Section of Low-Pressure Blades of Large Steam Turbines by Means of Cascade Tests

Stratford B. S. Sansome G. E. ‘The performance of supersonic turbine nozzles’, Rep. and Mentor. H.M.S.O. No. 3273.

Anon. ‘Tables of compressible airflow’, 1952. Prepared on behalf of the Aeronautical Research Council (Clarendon Press, Oxford).

Hauser C. H. Plohr H. W. Sondu G. ‘Study of flow conditions and deflection angle at exit of two-dimensional cascade of turbine rotor blades at critical and supercritical pressure ratios,’ 1950 Rep. and Mentor. N.A.S.A. No. E9K25.

Pearcey H. H. ‘The effect of condensation of atmospheric water vapour on total head and other measurements in N.P.L. high speed tunnel’, Rep. and Mentor. H.M.S.O. No. 2249.