Matches in SemOpenAlex for { <https://semopenalex.org/work/W789426586> ?p ?o ?g. }
Showing items 1 to 80 of
80
with 100 items per page.
- W789426586 abstract "The problem of a long, thin cylinder on a core, subjected to a finite band of axisymmetric radial load is considered. The core is analysed by elasticity theory. The cylinder is analysed by thin-shell theory. Appropriate displacements and stresses are matched at the cylinder-core interface. After careful numerical evaluation of improper integrals, which appear in the solution, non-dimensional displacement and stress ratios for the core and cylinder are presented for different widths of uniform pressure band load. A comparison to existing solutions for the limiting case of a line load is made and shows the maximum radial stress to be significantly larger than previously reported. It is also found that an increase in the band width from the limiting case of a line load decreases the stresses and displacements in the assembly significantly even though the external resultant force in kept constant. Introduction In recent years the development of solid propellant rocket technology has been very rapid. Considerable attention has been given to the structural safety and reliability of the motor case and its contents, which are a major component of such rockets. The present investigation is concerned with the effect of a uniform band of load intensity p and width 26 applied to a motor case assembly, as shown in Figure 1. Such a loading may arise when a clamp is placed over the assembly. The motor case is taken as a long, thin cylinder and its contents, consisting of solid propellant grain, is taken as a long solid cylinder or core. The core and cylinder are assumed to behave elastically. The core is examined by the use of equations from the theory of elasticity and the cylinder by the use of equations from classical thin shell theory. The elasticity equations for the core will be written in terms of displacements and solved with the aid of displacement functions. The shell theory equations" @default.
- W789426586 created "2016-06-24" @default.
- W789426586 creator A5021371505 @default.
- W789426586 creator A5024767693 @default.
- W789426586 creator A5028842236 @default.
- W789426586 date "1968-12-01" @default.
- W789426586 modified "2023-09-27" @default.
- W789426586 title "Elastic analysis of a long thin cylinder and core subjected to axisymmetric radial loads" @default.
- W789426586 cites W1533058090 @default.
- W789426586 cites W2055370028 @default.
- W789426586 cites W2061301711 @default.
- W789426586 cites W2163260666 @default.
- W789426586 cites W2752932982 @default.
- W789426586 hasPublicationYear "1968" @default.
- W789426586 type Work @default.
- W789426586 sameAs 789426586 @default.
- W789426586 citedByCount "0" @default.
- W789426586 crossrefType "journal-article" @default.
- W789426586 hasAuthorship W789426586A5021371505 @default.
- W789426586 hasAuthorship W789426586A5024767693 @default.
- W789426586 hasAuthorship W789426586A5028842236 @default.
- W789426586 hasConcept C102019270 @default.
- W789426586 hasConcept C121332964 @default.
- W789426586 hasConcept C121854251 @default.
- W789426586 hasConcept C127413603 @default.
- W789426586 hasConcept C138885662 @default.
- W789426586 hasConcept C146978453 @default.
- W789426586 hasConcept C159985019 @default.
- W789426586 hasConcept C192562407 @default.
- W789426586 hasConcept C203311528 @default.
- W789426586 hasConcept C21036866 @default.
- W789426586 hasConcept C33026886 @default.
- W789426586 hasConcept C41895202 @default.
- W789426586 hasConcept C57879066 @default.
- W789426586 hasConcept C66938386 @default.
- W789426586 hasConcept C76737569 @default.
- W789426586 hasConcept C78519656 @default.
- W789426586 hasConceptScore W789426586C102019270 @default.
- W789426586 hasConceptScore W789426586C121332964 @default.
- W789426586 hasConceptScore W789426586C121854251 @default.
- W789426586 hasConceptScore W789426586C127413603 @default.
- W789426586 hasConceptScore W789426586C138885662 @default.
- W789426586 hasConceptScore W789426586C146978453 @default.
- W789426586 hasConceptScore W789426586C159985019 @default.
- W789426586 hasConceptScore W789426586C192562407 @default.
- W789426586 hasConceptScore W789426586C203311528 @default.
- W789426586 hasConceptScore W789426586C21036866 @default.
- W789426586 hasConceptScore W789426586C33026886 @default.
- W789426586 hasConceptScore W789426586C41895202 @default.
- W789426586 hasConceptScore W789426586C57879066 @default.
- W789426586 hasConceptScore W789426586C66938386 @default.
- W789426586 hasConceptScore W789426586C76737569 @default.
- W789426586 hasConceptScore W789426586C78519656 @default.
- W789426586 hasLocation W7894265861 @default.
- W789426586 hasOpenAccess W789426586 @default.
- W789426586 hasPrimaryLocation W7894265861 @default.
- W789426586 hasRelatedWork W164088259 @default.
- W789426586 hasRelatedWork W1971415261 @default.
- W789426586 hasRelatedWork W1975045277 @default.
- W789426586 hasRelatedWork W1982767225 @default.
- W789426586 hasRelatedWork W1989064805 @default.
- W789426586 hasRelatedWork W2005333294 @default.
- W789426586 hasRelatedWork W2009502795 @default.
- W789426586 hasRelatedWork W2040862082 @default.
- W789426586 hasRelatedWork W2046520545 @default.
- W789426586 hasRelatedWork W2081816843 @default.
- W789426586 hasRelatedWork W2083064265 @default.
- W789426586 hasRelatedWork W2097663924 @default.
- W789426586 hasRelatedWork W2107428871 @default.
- W789426586 hasRelatedWork W2153831300 @default.
- W789426586 hasRelatedWork W2185249265 @default.
- W789426586 hasRelatedWork W2271819660 @default.
- W789426586 hasRelatedWork W300317717 @default.
- W789426586 hasRelatedWork W747713794 @default.
- W789426586 hasRelatedWork W2185433312 @default.
- W789426586 hasRelatedWork W304936043 @default.
- W789426586 isParatext "false" @default.
- W789426586 isRetracted "false" @default.
- W789426586 magId "789426586" @default.
- W789426586 workType "article" @default.