Using the linearized theory, calculate the lift and wave-drag coefficients for an infinitely thin flat plate in a Mach 2.6 freestream at angles of attack of(a) α = 5◦ (b) α = 15◦ (c) α = 30◦Compare these approximate results with those from the exact shockexpansion theory. What can you conclude about the accuracy of linearized theory in this case?
Using the linearized theory, calculate the lift and wave-drag coefficients for an infinitely thin flat plate in a Mach 2.6 freestream at angles of attack of(a) α = 5◦ (b) α = 15◦ (c) α = 30◦Compare these approximate results with those from the exact shockexpansion theory. What can you conclude about the accuracy of linearized theory in this case?
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Using the linearized theory, calculate the lift and wave-drag coefficients for an infinitely thin flat plate in a Mach 2.6 freestream at angles of attack of
(a) α = 5◦ (b) α = 15◦ (c) α = 30◦
Compare these approximate results with those from the exact shockexpansion theory. What can you conclude about the accuracy of linearized theory in this case?
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