Design of vertical open-throat wind tunnel built mainly for studying spinning characteristics of airplane models, but used as well for usual type; special spinning balance developed to measure forces and moments with model simulating actual spin; comparisons of results of stable autorotation and of rolling-moment tests obtained both in vertical tunnel and in old horizontal.
Vertical wind tunnel of national advisory committee for aeronautics
Nat. Advisory Committee Aeronautics -- Report
1931
10 pages
12 Figs.
Report
English
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The variable density wind tunnel of the national advisory committee for aeronautics
Engineering Index Backfile | 1926
|7 by 10 foot wind tunnel of National Advisory Committee for Aeronautics
Engineering Index Backfile | 1931
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