A technique is described for the analytical representation of the geometry of radial a~ld mixed flow compressor impellers constructed of radial or non-radial blade elements. A similar analytical expression is used to describe the hub, shroud, and camberline curves; if required, the angle of inclinat
โฆ LIBER โฆ
Computer-aided design of radial and mixed flow turbomachinery
โ Scribed by R.C. Atkey; D.S. Eastes; F.J. Wallace; A. Whitfield
- Publisher
- Elsevier Science
- Year
- 1974
- Tongue
- English
- Weight
- 175 KB
- Volume
- 6
- Category
- Article
- ISSN
- 0010-4485
No coin nor oath required. For personal study only.
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