Trimmed drag and maximum flight efficiency of aft tail and canard configurations
12th Aerospace Sciences Meeting ; 1974 ; Washington , DC , U.S.A.
1974-01-01
Conference paper
Electronic Resource
English
Minimum Induced Drag of Canard Configurations
AIAA | 1982
|Induced drag prediction for wing-tail and canard configurations through numerical optimisation
Online Contents | 1994
|AIAA | 1977
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