By utilizing the streamwise vector i parallel for the freestream in place of k in the integral, we obtain an expression with the tension drag Dp (which includes the tension part of the profile drag and, When the wing is a few-dimensional, the induced drag). If we utilize the spanwise https://raymondwdint.rimmablog.com/32615418/5-tips-about-motorized-garage-storage-lift-you-can-use-today