An edition of The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges (1952)

The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges

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The stability under longitudinal compression ...
Paul Seide
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Last edited by MARC Bot
December 19, 2022 | History
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An edition of The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges (1952)

The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges

by

  • 0 Ratings
  • 0 Want to read
  • 0 Currently reading
  • 0 Have read

A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.

Publish Date
Publisher
National Advisory Committee for Aeronautics
Language
English
Pages
30

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Subjects
Plates (Engineering), Sandwich construction, Loads (Mechanics), Buckling (Mechanics), Elasticity, Plaques (Ingénierie), Construction sandwich, Charges, Flambage (Résistance des matériaux), Élasticité, Warping, Buckling, Modulus of elasticity

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Cover of: The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges
The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges
1952, National Advisory Committee for Aeronautics
in English
  • Not in Library
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Book Details

Edition Notes

"Langley Aeronautical Laboratory.”

Date of issue: April 1952.

Report no. NACA-TN-2679.

Includes bibliographical references (page 19)

Published in
Washington, D.C
Series
National Advisory Committee for Aeronautics -- 2679, Technical note (United States. National Advisory Committee for Aeronautics) -- no. 2679.

Classifications

Dewey Decimal Class
624.17765
Library of Congress
TA660.P6

The Physical Object

Pagination
1 online resource (30 pages)
Number of pages
30

ID Numbers

Open Library
OL44477764M
ISBN 10
1680156241
ISBN 13
9781680156249
OCLC/WorldCat
919140207

Source records

marc_columbia MARC record

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December 19, 2022 Created by MARC Bot import new book