@article{oai:nagoya.repo.nii.ac.jp:00030958,
 author = {Otsuka, Shintaro and Aoki, Takashi},
 issue = {2},
 journal = {Memoirs of the Faculty of Engineering, Nagoya University},
 month = {Mar},
 note = {The fact, that there exists a relationship between the turning angle and the axial velocity ratio which depends only on the inflow angle, inflow boundary layer thickness and aspect ratio, but is independent of the pitch chord ratio and stagger angle on the solid wall compressor cascade experiment, was clarified, and an experimental equation was derived from experimental data.},
 pages = {236--244},
 title = {The relation between turning angle and axial velocity ratio of solid wall compressor cascades},
 volume = {26},
 year = {1975}
}