Investigation made at request of Navy Bureau of Aeronautics for determining maximum loads during violent maneuvers; existing loading specifications do not conform satisfactorily to loadings existent in critical conditions; in some cases exceeded; acceleration of 10.5 g. recorded in one maneuver in which pilot suffered severely; limits of physical resistance of pilot to violent maneuvers being approached; Navy specifications for structural design included.
The pressure distribution over the horizontal and vertical tail surfaces of the f6c-4 pursuit airplane in violent maneuvers
Nat. Advisory Committee Aeronautics -- Report
1929
20 pages
29 Figs.
Report
English
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Engineering Index Backfile | 1930
|The pressure distribution over the horizontal tail surfaces of an airplane
Engineering Index Backfile | 1921