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NACA-TR-748

Normal Pressure tests of Rectangular Plates

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:09:08Z
date available2017-09-04T16:09:08Z
date copyright01/01/1942
date issued1942
identifier otherSFYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/72374
description abstractReport presents the results of normal-pressure tests made of 56 rectangular plates with clamped edges and of 5 plates with freely supported edges. Pressure was applied and the center deflection and the permanent set at the center were measured. For some of the plates, in addition, strains and contours were measured.
languageEnglish
titleNACA-TR-748num
titleNormal Pressure tests of Rectangular Platesen
typestandard
page29
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsAIRCRAFT LANDING
subject keywordsALUMINUM ALLOYS
subject keywordsCLAMPS
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsDEFLECTION
subject keywordsEDGES
subject keywordsELASTIC PROPERTIES
subject keywordsFLAT PLATES
subject keywordsIMPACT LOADS
subject keywordsPRESSURE EFFECTS
subject keywordsRECTANGULAR PLATES
subject keywordsSTAINLESS STEELS
subject keywordsSTRESS-STRAIN RELATIONSHIPS
subject keywordsSUPPORTS
subject keywordsTENSILE PROPERTIES
subject keywordsWATER TAKEOFF AND LANDING AIRCRAFT


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