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.
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Emerald Group Publishing | 1931
|Numerical simulation of wing-fuselage interference
AIAA | 1982
|Numerical simulation of wing-fuselage interference
AIAA | 1981
|Minimum induced drag in wing-fuselage interference
TIBKAT | 1941
|