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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
why we need EJB
Q. Distinguish between Fresnel's and Fraunhofer's classes of diffraction. Show that the relative intensities of successive maxima of Fraunhofer diffraction at single slit are
briefly differenciate the moore & mealy machines
apply equations to solve problems for specified aerodynamic applications. Need some inputs regarding this.
assignment
what are clippers
Constant speeding propeller: The definition of a Constant Speeding propeller is 'A propeller, the pitch setting of which varies automatically to maintain a preselected constant
Hi, i want to get a quote for my communication networks assignment
I am having difficulty with algebra pertaining toengineering
Please help me to compare the minimum cell cost method and Vogel''s approximation method to find initial basic solution. Generally the sources indicated that the Vogel''s method gi
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