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)
Book Details
Author(s)Aeronautical Research Council
PublisherH.M.S.O
ISBN / ASINB0000CIFH3
ISBN-13978B0000CIFH2
Sales Rank99,999,999
MarketplaceUnited States 🇺🇸

