Rutgers University 3 credits Mechanical and Aerospace Engineering
Basic concepts in aerospace engineering; pressure, density, temperature, atmosphere, NACA and NASA, equation of state, airfoils, streamlines, standard atmosphere, interpolation and use of data; basic aerodynamics, continuity equation, Bernoulli's equation, streamlines, lift and drag, Reynolds number, flow separation, boundary layer, drag coefficient; airfoil nomenclature, quarter chord point NACA charts, finite wingspan, aspect ratio, drag polar, summary of drag effects; aircraft performance, required thrust and power, rate of climb, gliding, take-off and landing performance, turning; aircraft equations and stability, effects of wings and tail; astronautics, Newton's law of gravitation, polar coordinates, orbital motion, momentum and energy, types of orbits, escape velocity, Kepler's laws, earth satellites, launch window, reentry dynamics; ballooning. Prerequisites: 01:640:152 and 14:440:221 (or 14:440:291).
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