Effect of normal pressure on the critical compressive and shear stress of curved sheet
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Author
Contributions
- Sandlin, Charles W. - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1945 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- ISBN-101680156357
- ISBN-139781680156355
- OCLC Control Number914330037
- Open LibraryOL44477661M
Classifications
- DDC624.17723
- LCCTA660.B4
Alternate Titles
- NACA Wartime Reports. Series L.
Description
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure.
Subjects
Topics
StressStrainChargesWarpingAlliagesBucklingDiagramsAluminiumBox beamsCurvatureShear stressAluminum alloyAluminum alloysCharts, diagramsPoutres-caissonsLoads (Mechanics)Shear (Mechanics)Strains and stressesTableaux, graphiquesPlates (Engineering)Buckling (Mechanics)Contraintes (Mécanique)Cisaillement (Mécanique)Flambage (Résistance des matériaux)
Series Statement
- Wartime Report / National Advisory Committee for Aeronautics -- no. L57
- Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L57.
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