Study of the Stall-Spin Phenomena Using Analysis and Interactive 3-D Graphics
Author: Dubois, Pascale Claude
Year: 1986
Degree: Engineer's thesis
Advisor: Culick, Fred E. C.
Committee Members: Culick, Fred E. C.; Roshko, Anatol; Liepmann, Hans Wolfgang
Option: Aeronautics
DOI: 10.7907/SFMF-Z114
Abstract
The purpose of this study is to gain a better understanding of the nonlinear stall-spin phenomenon through numerical analysis and interactive 3-D graphics.
The linear aerodynamic range was thoroughly examined for the NAVION, a light aviation aircraft. Nonlinear aerodynamic behavior was modeled by adding nonlinearities to the lift, pitching and rolling moments. The results of this analysis are promising; however, a more sophisticated model is needed to fully simulate the stall-spin phenomenon.
A graphic tool is described which allows the user to interact with the simulation process. This gives the user a "feel" for the dynamics of aircraft and effectively displays the characteristic features of the dynamic model.
Files
- Dubois_pc_1986.pdf (application/pdf)