Interpretation of available test data points to conclusions favorable to high wing in monoplanes. Reprinted from Aeronautical Research Committee R and M. no. 1344, price 9 d.
Fuselage interference effect
Aircraft Eng
Aircraft Engineering ; 3 , n 30
1931
3 pages
2 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
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