Dynamic stall constitutes a major limiting factor for helico-pter's forward speed. Calculations of rotor airloads and helicopter limiting speeds introducing the blade pitching oscillations effects, translate the real case into a reasonable analytical model. The present technique offers a reliable mean for calculating the rotor airloads with the unsteady effects. The method is extended to determine the limiting forward speed of helicopter.
TALAAT, E., & KATARY, M. (1985). DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE. International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), 255-265. doi: 10.21608/asat.1985.26480
MLA
E. TALAAT; M. A. KATARY. "DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE", International Conference on Aerospace Sciences and Aviation Technology, 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, 1985, 255-265. doi: 10.21608/asat.1985.26480
HARVARD
TALAAT, E., KATARY, M. (1985). 'DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE', International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), pp. 255-265. doi: 10.21608/asat.1985.26480
VANCOUVER
TALAAT, E., KATARY, M. DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE. International Conference on Aerospace Sciences and Aviation Technology, 1985; 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO): 255-265. doi: 10.21608/asat.1985.26480
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