OPTIMIZING NACA AIRFOIL THICKNESS FUNCTION PARAMETERS FOR MAXIMUM LIFT-TO-DRAG RATIO
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
2020
Aufsatz (Konferenz)
Englisch
Lift and Drag Control of NACA 23012 Airfoil Model by Surface HF Plasma Actuator (AIAA 2014-1263)
British Library Conference Proceedings | 2014
|Engineering Index Backfile | 1944
|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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