Problem Set, Assignment, and Solutions
To introduce aviation/aeronautics/aerospace students to wind tunnel(s) and methods used in experimental identification of various aerodynamic (and stability) coefficients of airfoils (2D), wings (3D) and scale models.
Daidzic, N. E. (2020). AVIA 201 Project 1 Windtunnel Lab Form Ver 1.20 20200323. Minnesota State University, Mankato. https://works.bepress.com/nihad-daidzic/91/
Aerodynamics and Fluid Mechanics Commons, Algebra Commons, Aviation and Space Education Commons