Experimental Poststall Rotary Aerodynamic Coefficients for Airplane-like Configurations
- 1 August 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (8) , 565-570
- https://doi.org/10.2514/3.58688
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling: Part 11-Nonlinear Coning-Rate DependenceAIAA Journal, 1975
- Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolutionAIAA Journal, 1970