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Question
A model airplane has a wing span of 3.1 ft and a chord (leading edge–trailing edge distance) of 5 in. The model flies in air at 60 and atmospheric pressure. The wing can be regarded as a flat plate so far as drag is concerned. (a) At what speed will a turbulent boundary layer start to develop on the wing? (b) What will be the total drag force on the wing just before turbulence appears?
Solution
VerifiedAnswered 1 year ago
Answered 1 year ago
Step 1
1 of 7Given:
Air at and
Wing Span,
Leading Edge Distance,
Required:
Velocity at which Turbulence starts to occur,
Drag Force on Wing,
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