Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated ice
- 1 February 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (2) , 130-134
- https://doi.org/10.2514/3.45096
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Aerodynamic evaluation of a helicopter rotor blade with ice accretion in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Performance degradation of a model helicopter main rotor in hover and forward flight with a generic ice shapePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Experimental study of performance degradation of a model helicopter main rotor with simulated ice shapesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Helicopter rotor performance degradation in natural icing encounterJournal of Aircraft, 1984
- Performance degradation of propeller systems due to rime ice accretionJournal of Aircraft, 1984
- Aerodynamic characteristics of airfoils with ice accretionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982