Zobrazeno 1 - 2
of 2
pro vyhledávání: '"Kailash Sunneechurra"'
Autor:
William Crowther, Kailash Sunneechurra
Publikováno v:
Journal of Aircraft. 44:1052-1055
T HE leading-edge high-lift system on a typical transport aircraft wing typically contributes 2–3% to the overall wing weight. There is therefore considerable incentive to explore leading-edge flow control solutions that could approach the performa
Publikováno v:
Scopus-Elsevier
1 , the velocity ratio between the freestream and the exit peak velocity of the jet was set to 1.2, the Strouhal number to 0.069 and the boundary layer thickness was measured to be 9 times the diameter of the orifice. Differences in the roll-up proce