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"Behavior of a cylindrical shell under axial compression when the buckling load has been exceeded." Source: Royal Aircraft Establishment. Report SME 3204

National Air and Space Museum

Object Details

sova.nasm.xxxx.0428_ref6368
GUID
https://n2t.net/ark:/65665/pg2a1253eac-aab1-4e9c-aa0a-496287b10014
Collection Creator
Wright-Patterson Air Force Base (Ohio)
See more items in
Wright Field Technical Documents Library
Wright Field Technical Documents Library / D50. Transportation, Supplies, and Equipment / D52. Aircraft / D52.16 - Aircraft Design and Construction
Date
Aug 1942
Container
Box D696, Folder D52.16 / 365
Archival Repository
National Air and Space Museum Archives
Type
Archival materials
Collection Rights
Material is subject to Smithsonian Terms of Use. Should you wish to use NASM material in any medium, please submit an Application for Permission to Reproduce NASM Material, available at Permissions Requests
Scope and Contents
Leggett, D.M.A.; Jones, R.P.N.; Royal Aircraft Establishment - Report S.M.E. 3204; jt, auth.; Shells; Stresses
Collection Restrictions
No restrictions on access
NASM.XXXX.0428_ref6368
Large EAD
https://n2t.net/ark:/65665/pg2a1253eac-aab1-4e9c-aa0a-496287b10014
NASM.XXXX.0428
NASMAC
Record ID
ebl-1679568301227-1679568346185-1

  • Wright Field Technical Documents Library


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