With reference to problem of rotating compressor stall, unsteady boundary layer calculation is made to find unsteady increment of lift of stalled elliptic airfoil in flow of time dependent incidence.
Lift hysteresis at stall as unsteady boundary-layer phenomenon
NACA -- Tech Note
1955
32 pages
Report
English
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Unsteady Flow Simulation of High-Lift Stall Hysteresis Using a Lattice Boltzmann Approach
British Library Conference Proceedings | 2012
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