Experiments on a 20 per cent. control with tab, fitted to NACA 0015 aerofoil, with especial reference to effect of its section on hinge moment and lift
1949
27 S.
Report
English
Effect of Piezoelectric Actuation on a NACA 0015 Aerofoil at Subsonic Speeds (AIAA 2006-0103)
British Library Conference Proceedings | 2006
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