Wind tunnel tests at mach numbers up to 1, 8 on a model with 1, 36 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188) (Current papers; no.798)
Book Details
Author(s)Aeronautical Research Council
PublisherH.M.S.O
ISBN / ASINB0000CMKZ2
ISBN-13978B0000CMKZ2
MarketplaceGermany 🇩🇪
