The drag of an airfoil at zero angle of attack is a function of density, viscosity, and velocity, in addition to a length parameter



Download 2.42 Mb.
Page12/31
Date20.05.2018
Size2.42 Mb.
#49465
1   ...   8   9   10   11   12   13   14   15   ...   31

since p varies only in the s-direction
Newton’s law of fluid viscosity:


Download 2.42 Mb.

Share with your friends:
1   ...   8   9   10   11   12   13   14   15   ...   31




The database is protected by copyright ©ininet.org 2024
send message

    Main page