Procedure developed for calculation of structural response of airplane subject to dynamic loads; particular attention given to problem of determining stresses developed due to flight through gusts. (see also J Aeronautical Sciences v 17 n 9 Sept 1950 p 540-50, 594)
Recurrence matrix solution for dynamic response of aircraft in gusts
Nat Advisory Committee Aeronautics -- Tech Note
1950
90 pages
Diagrs, Tables
Report
English
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Recurrence matrix solution for dynamic response of aircraft in gusts
Engineering Index Backfile | 1950
|Recurrence matrix solution for dynamic response of aircraft in gusts
Engineering Index Backfile | 1951
|