Wind-tunnel investigation of effect of yaw on lateral-stability characteristics II, Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin /
| Main Authors: | , |
|---|---|
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, [D.C.] :
National Advisory Committee for Aeronautics,
1939
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
730 |
| Subjects: |