Structural design of cabane struts for the PW-1 with R. A. F. 15 taped wings (airplane section, S. & A. branch)

United States. Army. Air Service. Engineering Division.

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asic172_ocr.pdf (6.228Mb)

Date

1921-01-15

Author

United States. Army. Air Service. Engineering Division.

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Description

This document describes investigation of stresses in cabane struts under three conditions of loading: high incidence, low incidence, and reversed flight.

URI

http://hdl.handle.net/11200/49120

Collections

Air Service Information Circulars