✦ LIBER ✦
Possible extension of pre-stall limits for flows in a compressor aerofoil blade row by fractal compatability with topography in a feedback channel
✍ Scribed by B.S. Thornton; L.C. Botten; J.P. Gostelow
- Publisher
- Elsevier Science
- Year
- 1991
- Tongue
- English
- Weight
- 240 KB
- Volume
- 156
- Category
- Article
- ISSN
- 0375-9601
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