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Low speed wind tunnel test of a propulsive wing/canard concept in the STOL configuration (SuDoc NAS 1.26:178348-178349)

Author V. R. Stewart
Publisher National Aeronautics and Space Administration, Langley Research Center
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Book Details
Author(s)V. R. Stewart
ISBN / ASINB000105DF6
ISBN-13978B000105DF4
Sales Rank99,999,999
MarketplaceUnited States 🇺🇸