This book describes an engineering approach based on interactive boundary-layer and stability-transition theories, both developed by the author, for calculating aerodynamic flows. This is the first time these powerful computational techniques have been published in book form.3, Hot-Wire and Hot-Film Measurements. NASA TM 84245.  Ruff, G.A. and Berkowitz, B.M., aquot;Usera#39;s Manual for the NASA Lewis Ice Accretion Code (LEWICE ), aquot; NASA CR-185129, May 1990.  Bragg, M.B. and Coirier, W.J., aquot; Aerodynamicanbsp;...
|Title||:||An Engineering Approach to the Calculation of Aerodynamic Flows|
|Publisher||:||Springer Science & Business Media - 1999-11-05|