Results of tests made in 1918 in old 4-ft. wind tunnel at Mass. Inst. of Technology, for purpose of securing data on effect of windshield form on total resistance of fuselage of good streamline shape.
Wind tunnel tests of fuselages and windshields
U.S. Nat. Advisory Comm. Aeronautics -- Tech. Notes
1925
6 pages
4 Figs. on supp. plates
Report
Englisch
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Wind tunnel tests of fuselages and windshields
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