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)

Name: 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)
Author: Aeronautical Research Council
ISBN: 978B0000CMKZ2

Author Aeronautical Research Council

Publisher H.M.S.O

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Book Details

Author(s)Aeronautical Research Council

PublisherH.M.S.O

ISBN / ASINB0000CMKZ2

ISBN-13978B0000CMKZ2

MarketplaceIndia 🇮🇳