Stress analysis of Lieut. Phillips' 'Alouette' airplane (airplane section report)
Newell, J. S.
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DescriptionThe following report covers the analysis of the wing, fuselage, and landing gear structures of the Alouette airplane. This analysis was made in order to determine the structural safety of the airplane ... As a result of this analysis it is concluded that the primary structure of this airplane, with the exception of the landing gear, is safe. ... These unsatisfactory portions of the structure can be easily changed and brought up to the desired strength.
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