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The cl,max for the NACA LS (1) – 0417 is higher than that for the NACA 2412.
Consider a NACA 2812 airfoil. It is operating with flow velocity of 900m/s with chord of 1m. What should be the maximum thickness of this airfoil?
An airfoil is such that the drag produced by airfoil is 25N. Airfoil has chord of 2m and is experiencing dynamic pressure of 10Pa. Find the value of drag co-efficient for airfoil.
The NACA LS (1) – 04XX airfoils when compared to NACA airfoils with same thickness had higher L/D ratios. For a lift coefficient of 1.0, what was this increase approximately in percentage?
Why NACA 0012 airfoil is said to be symmetric airfoil?
Which is not a feature of the first new NACA airfoil (GA(W)-1 or the Whitcomb airfoil) developed?
How is supercritical airfoil different from the NACA 64 series airfoil?
Thickness of 8 tyres L, M, N, O, P, Q, R and S is compared. Thickness of no two tyres is same. Thickness of N is more than L but less than 6 tyres. Thickness of O is more than M but less than Q. Thickness of P is less than only two tyres. Thickness of Q is not more than P. Which of the following statement is not correct?
What is the thickness in NACA 747A315 airfoil?
What is the thickness of NACA 0002 airfoil?