Tests concerning novel designs of blades for axial compressors
1956
22 S.
graph. Darst.
Enth.: Part 1. Blades designed for increased work at root and tip. - Part 2. Blades designed to operate in a parabolic axial velocity distribution
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Shock-Loss Model for Transonic and Supersonic Axial Compressors with Curved Blades
Online Contents | 1998
|CASCADE ANALYSIS AND DEVELOPMENT OF NEW TANDEM BLADES FOR AXIAL FLOW COMPRESSORS
British Library Conference Proceedings | 2009
|