Conclusions approved by subcommittees on determination of mechanical resistance of airplanes; includes (1) determination of main conditions entailing overload and examination of existing theoretical and experimental data; (2) reduction of general conditions of calculation to some simple cases; (3) determination of load factors to be adopted in each of these cases; (4) methods of control, known as static tests. Supp. to Bul. de la Chambre Syndicale des Industries Aeronautiques.
Permanent Commission of Aeronautical Studies report no. 4
Nat. Advisory Committee Aeronautics -- Tech. Memorandums
1927
19 pages
Report
Englisch
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