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Fluid mechanics / Drag divergence Mach number / Airfoil / Supercritical airfoil / Drag / Lift / Pressure coefficient / Camber / Mach number / Aerodynamics / Aerospace engineering / Fluid dynamics


MACH NUMBER, RELATIVE THICKNESS, SWEEP AND LIFT COEFFICIENT OF THE WING – AN EMPIRICAL INVESTIGATION OF PARAMETERS AND EQUATIONS D. Scholz, S. Ciornei Hamburg University of Applied Sciences Department of Automotive and
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Document Date: 2005-10-26 05:29:51


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File Size: 1,00 MB

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