Document Type
Problem Set, Assignment, and Solutions
Publication Date
3-23-2020
Abstract
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.
Department
Aviation
Recommended Citation
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/
Included in
Aerodynamics and Fluid Mechanics Commons, Algebra Commons, Aviation and Space Education Commons
