Abstract
Results of a comparison of dynamic stall onset are presented, as assessed from low Mach number windtunnel data contained in the University of Glasgow's database and that from the well established Beddoes' model. The model, which was originally developed to reconstruct higher Mach number dynamic stall characteristics, exhibited a lower stall onset incidence than that assessed from the windtunnel data. The differences and speculations on the physical reasoning underlying the two assessments are discussed. An addition to the Beddoes model is proposed which yields an improved reconstruction of the Glasgow windtunnel data.
Original language | English |
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Pages | 67-76 |
Number of pages | 10 |
Volume | 101 |
No. | 1002 |
Specialist publication | Aeronautical Journal |
Publication status | Published - Feb 1997 |