Simplification of nonlinear indicial response models - Assessment for the two-dimensional airfoil case
- 1 February 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (2) , 131-138
- https://doi.org/10.2514/3.46001
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Two dimensional post stall maneuver of a NACA 0015 airfoil at high pitching ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flowJournal of Aircraft, 1988
- Nonlinear aerodynamics of two-dimensional airfoils in severe maneuverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988