A short method of calculating torsional stresses in an airplane fuselage /
Saved in:
Author / Creator: | Younger, John E. (John Elliott), 1892- author. |
---|---|
Imprint: | [Washington, D.C.] : National Advisory Committee for Aeronautics, 1924. |
Description: | 1 online resource (23 pages, 6 unnumbered pages) : illustrations. |
Language: | English |
Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 203 Technical note (United States. National Advisory Committee for Aeronautics) ; 203. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12316466 |
Other authors / contributors: | United States. National Advisory Committee for Aeronautics, issuing body. |
---|---|
Notes: | "September, 1924." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references. Description based on online resource, PDF version; title from title page (TRAIL, viewed April 22, 2020). |
Other form: | Print version: Younger, John E. Short method of calculating torsional stresses in an airplane fuselage |
GPO item no.: | 9999 (online) |
Govt.docs classification: | Y 3.N 21/5:6/203 |
Similar Items
-
Application of double Fourier series to the calculation of stresses caused by pure bending in a circular monocoque cylinder with a cut-out,
by: Krzywoblocki, Zbigniew, 1904-1978
Published: (1946) -
Drag of exposed fittings and surface irregularities on airplane fuselages /
by: Wood, Donald H
Published: (1928) -
Structural weight analysis: fuselage and shell structures. Jan., 1950. R-172.
by: Micks, William Raymond, 1923-
Published: (1950) -
Investigation of fire resistance of aircraft fuselages /
by: Hutton, A. C.
Published: (1952) -
Bending tests of metal monocoque fuselage construction /
by: Mossman, Ralph W.
Published: (1930)