Results of investigation of effects of changes in elevator and rudder settings and of small changes in attitude upon aerodynamic forces and moments exerted upon spinning airplane undertaken with spinning balance in 5-ft vertical tunnel of National Advisory Committee for Aeronautics.
Aerodynamic forces and moments exerted on spinning model of "NY-1" airplane as measured by spinning balance
Nat Advisory Committee Aeronautics -- Report
1933
15 pages
Report
English
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Aerodynamic forces and moments on spinning model of F4B-2 airplane as measured by spinning balance
Engineering Index Backfile | 1935
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