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Unformatted text preview: V Â¶ The resulting plot is shown below. AA311  Atmospheric Flight Mechanics Christopher Lum Printed by Mathematica for Students Part b. With knowledge of the maximum climb angle, the rate of climb is given by RoC = V Â¶ sin H q max L We can compare this with Eq.6.50 which is an approximation of rate of climb. The results are shown below 2 hw08_solutions.nb Printed by Mathematica for Students As can be seen, Eq.6.50 is a good approximation at low climb angles. hw08_solutions.nb 3 AA311  Atmospheric Flight Mechanics Christopher Lum Printed by Mathematica for Students Problem 2 Not applicable. 4 hw08_solutions.nb Printed by Mathematica for Students...
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 Fall '09
 Numerical Analysis, Power, Aerodynamics, Optimization, Pick operating system

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