Show simple item record

NASA-TN-D-402

Analysis of frame-reinforced cylindrical shells. Part III - Applications

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:54:19Z
date available2017-09-04T15:54:19Z
date copyright01/01/1960
date issued1960
identifier otherQRTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/57611
description abstractThere are basically two approaches to determining stresses that are due to concentrated loads applied to flexible frames which are supported by cylindrical shells. One is to make a complete redundant analysis of each problem, utilizing a large digital computer. The second, which is adopted here, is to devise simple approximate procedures. Such procedures should promote a better understanding of the problem, and provide tables or charts of results as functions of as few parameters as practicable. The analysis is undertaken in references 1 and 2. The results obtained from that analysis are summarized in this report which is intended to be a reference for persons interested in using the results, but who are not concerned with the mathematical derivations.
languageEnglish
titleNASA-TN-D-402num
titleAnalysis of frame-reinforced cylindrical shells. Part III - Applicationsen
typestandard
page137
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsANALYSIS
subject keywordsCYLINDRICAL
subject keywordsDATA
subject keywordsDISPLACEMENT
subject keywordsDISTRIBUTION
subject keywordsFORCES
subject keywordsLOADS
subject keywordsMATHEMATICAL
subject keywordsMODELS
subject keywordsMOMENT
subject keywordsNONUNIFORMITY
subject keywordsRADIAL
subject keywordsREINFORCED
subject keywordsSHELLS
subject keywordsSTRESS
subject keywordsTABLES


Files in this item

Thumbnail
Name:
QRTKAEAAAAAAAAAA.pdf
Size:
2.523Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record