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
Publisher
H.M.S.O
ISBN / ASIN
B0000CIFH3
ISBN-13
978B0000CIFH2
Marketplace
United States 🇺🇸
