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PDF) Computation of flow through transonic axial compressor cascade, for the blade with non-linear load and non-linear tangent velocity radial design, by using the active disk theory
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Compressor Aerodynamics. By N. A. CUMPSTY. Longman, 1989. 509 pp. £49. | Journal of Fluid Mechanics | Cambridge Core
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aerodynamics - Why is a centrifugal compressor in aircraft engine less susceptible to stall and surge? - Aviation Stack Exchange
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