Linearized theory of supercavitating flow through an arbitrary form hydrofoil.
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概要
Institute of High Speed Mechanics, Tohoku University | 論文
- Ultraschallwelle am Tragflugelprofil bei Hohsog,Teil 3.
- Boundary layer thickness of converging nozzle.
- Method to get profile of nozzle with given velocity distribution along nozzle axis,1.
- Postbuckling behavior of rectangular plates with small initial curvature loaded in edge compression,2.
- Bending of stiffened plates under uniform normal pressure.