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Design Features of Supercritical Aerofoil
• Blunt nose-
rapid p pressure reduction around leading edge
• Flat top-
Reduce the flow acceleration on upper surface toreduce shock strength
• Cusped trailing edge-
Increased loading over rear of aerofoil to recoversome lift
Velocity vector
Speed of NACA
#include org 0xoo movlw 0x00 ---------- movlw 0xff movwf PORTB end
The load data given in Table 1 belongs to a power company. Develop the daily load curve for the primary feeder. Also, determine: a. maximum coincident demand of the system b. deman
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Comparison of FP result with experiment At the lowest test lift coefficient the flow is just subcritical (in the sense that the Mach number of the flow component normal to the
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