Investigation of specific tail configuration in Langley 15-ft free spinning tunnel.
Hinge-moment characteristics of balanced elevator and rudder for specific tail configuration on fuselage in spinning attitudes
Nat Advisory Committee Aeronautics -- Tech Note
1947
11 pages
13 Supp Sheets
Report
English
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Rudder piece hinge moment adjusting method, hinge moment adjustable rudder piece and control method
European Patent Office | 2025
|Engineering Index Backfile | 1947
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