onsider a 118 m/s airflow over a flat plate that is 1.1 m long perpendicular to the freestream direction. The freestream conditions correspond to standard sea level values. Assuming turbulent flow all throughout, calculate the total skin friction drag if the turbulent boundary layer has a thickness of 1.37 x 10-3 m at the trailing edge. Provide answer in Newtons, and round it off to the nearest thousandths.

onsider a 118 m/s airflow over a flat plate that is 1.1 m long perpendicular to the freestream direction. The freestream conditions correspond to standard sea level values. Assuming turbulent flow all throughout, calculate the total skin friction drag if the turbulent boundary layer has a thickness of 1.37 x 10-3 m at the trailing edge. Provide answer in Newtons, and round it off to the nearest thousandths.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.50P

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