An air stream flows over a smooth plate with Reynolds number of 106. The boundary layer can be assumed to be turbulent over the entire plate. If the length of the plate is increased by 10%, taking all the factors same, what is percentage change in the total drag coefficient? [Take (1.1) 0.2 = 1.019]
An air stream flows over a smooth plate with Reynolds number of 106. The boundary layer can be assumed to be turbulent over the entire plate. If the length of the plate is increased by 10%, taking all the factors same, what is percentage change in the total drag coefficient? [Take (1.1) 0.2 = 1.019]
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![An air stream flows over a smooth plate with Reynolds number of 106. The boundary layer can
be assumed to be turbulent over the entire plate. If the length of the plate is increased by 10%,
taking all the factors same, what is percentage change in the total drag coefficient?
[Take (1.1)0.2 = 1.019]](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa1043704-e093-485d-8f4f-f0134460c3ae%2Fe5879244-aca6-4f06-b5ed-6ede76ab43cc%2Fexl8n4w_processed.jpeg&w=3840&q=75)
Transcribed Image Text:An air stream flows over a smooth plate with Reynolds number of 106. The boundary layer can
be assumed to be turbulent over the entire plate. If the length of the plate is increased by 10%,
taking all the factors same, what is percentage change in the total drag coefficient?
[Take (1.1)0.2 = 1.019]
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