1 edition of A wind tunnel test at M=1.39 of the increase in wave drag due to control surfaces in either tail or canard position on a Sears-Haack type of body found in the catalog.
A wind tunnel test at M=1.39 of the increase in wave drag due to control surfaces in either tail or canard position on a Sears-Haack type of body
1982 by Dept. of Aeronautics, The Royal Institute of Technology in Stockholm, Sweden .
Written in English
|The Physical Object|
|Number of Pages||10|
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