Investigations on an experimental air-cooled turbine.  Part III: The effects of cooling on the overall turbine aerodynamic performance and initial operation at an inlet gas temperature of 1400 deg K.  Part IV: Examination of sintered vitallium air-cooled turbine blades following 100 hours' operation at a turbine inlet mean gas temperature of 1400 deg K
By: D. E. Fray, N. E. Waldren and C. J. Hart.
Contributors: Hart, C. J.; Waldren, N. E.; Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council.  Reports and memoranda -- no. 3144
Publisher: Ministry of Aviation, Aeronautical Research Council
Published: 1960
Place of publication: London
Number of pages: 53
Notes: Bibliographical references: p. 35.