Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study.
[Part] I,
, Design and experimental performance of standard turbine /
Harold E. Rohlik, William T. Wintucky and Herbert W. Scibbe..

APA Citation

Rohlik, H. E., Scibbe, H. W., Wintucky, W. T., Lewis Flight Propulsion Laboratory., United States. National Adviosry Committee for Aeronautics., United States. National Advisory Committee for Aeronautics. (1957). Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study. Washington, D.C.: National Advisory Committee for Aeronautics.

MLA Citation

United States. National Advisory Committee for Aeronautics, et al.. Investigation of a 0.6 Hub-tip Radius-ratio Transonic Turbine Designed for Secondary-flow Study. Washington, D.C.: National Advisory Committee for Aeronautics, 1957.

Warning: These citations may not always be complete (especially for serials).