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The airfoil section of a horizontal tail in a GA aircraft is NACA 0012. The tail aspect ratio is 4.8. Using Ref. [8], calculate the
The airfoil section of a horizontal tail in a GA aircraft is NACA 0012. The tail aspect ratio is 4.8. Using Ref. [8], calculate the tail lift curve slope in 1/rad
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Fundamentals of Physics
Authors: Jearl Walker, Halliday Resnick
9th Edition
ISBN: 470469080, 470556536, 470469110, 9780470469088, 9780470556535, 978-0470469118
