A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps (SuDoc NAS 1.26:181684)

Name: A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps (SuDoc NAS 1.26:181684)
Author: Dhanvada M. Rao
ISBN: 978B0001050V4

Author Dhanvada M. Rao

Publisher National Aeronautics and Space Administration, Langley Research Center

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Book Details

Author(s)Dhanvada M. Rao

PublisherNational Aeronautics and Space Administration, Langley Research Center

ISBN / ASINB0001050VI

ISBN-13978B0001050V4

Sales Rank99,999,999

MarketplaceUnited States 🇺🇸