Note on the effect of compressibility on the profile drag of aerofoils at subsonic mach numbers in the absence of shock waves (Reports and memoranda series;no.2400)
Book Details
Author(s)Aeronautical Research Council
PublisherH.M.S.O
ISBN / ASINB0000CHPFN
ISBN-13978B0000CHPF2
Sales Rank99,999,999
MarketplaceUnited States 🇺🇸

