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4.11 The flying wing, B-2 stealth bomber can be approximated by a flat plate with dimensions...

4.11 The flying wing, B-2 stealth bomber can be approximated by a flat plate with dimensions of 69 f (chord) x 172 f (span).  It’s cruising at 25,000 f. Assume the flow over both sides of the bomber is completely turbulent.  The absolute viscosity coefficient is 5.2(10)-7 sl/f/s. Determine the total skin friction drag at Mach numbers 1.0, 2.0 and 3.0 for this airplane.

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