OPTIMIZING NACA AIRFOIL THICKNESS FUNCTION PARAMETERS FOR MAXIMUM LIFT-TO-DRAG RATIO
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
2020
Conference paper
English
Lift and drag data for 30 pusher-propeller shaft housings on NACA 65, 3-018 airfoil section
Engineering Index Backfile | 1943
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