Unformatted text preview: ft ], such that, when finished, the table will have 16 rows, and should include: (a) Altitude, h [ ft ] (b) Low Speed Solution, V Low [ ft/s ] (c) High Speed Solution, V High [ ft/s ] (d) Stall Speed, V Stall [ ft/s ] (e) Dynamic Pressure Speed, V QMax [ ft/s ] (f) Maximum Mach Number Speed, V MMax [ ft/s ] 6. Plot the low speed and high speed solutions on a plot of altitude vs. velocity. Add the dynamic pressure limit, the Mach number limit, and the stall limit curves to your plot to produce a flight envelope for the 11000 [ lb ] Lear Jet. Add a ceiling of h Max = 40000 [ ft ] to your flight envelope. As an added level of sophistication, use the fill command in MATLAB to automate the process of ¯lling the level flight envelope....
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 Spring '10
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 Fluid Dynamics, Aerodynamics, Velocity, impact pressure

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