Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per cent control, with especial reference to effect of curvature of control ... surface (Reports & memoranda series;no.2698)
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Book Details
Author(s)Aeronautical Research Council
ISBN / ASINB0000CIFH3
ISBN-13978B0000CIFH2
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