Virtual Principles in Aircraft Structures:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Dordrecht
Springer Netherlands
1989
|
| Schriftenreihe: | Mechanics of Structural Systems
6-7 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Beschreibung: | The basic partial differential equations for the stresses and displacements in clas sical three dimensional elasticity theory can be set up in three ways: (1) to solve for the displacements first and then the stresses; (2) to solve for the stresses first and then the displacements; and (3) to solve for both stresses and displacements simultaneously. These three methods are identified in the literature as (1) the displacement method, (2) the stress or force method, and (3) the combined or mixed method. Closed form solutions of the partial differential equations with their complicated boundary conditions for any of these three methods have been obtained only in special cases. In order to obtain solutions, various special methods have been developed to determine the stresses and displacements in structures. The equations have been reduced to two and one dimensional forms for plates, beams, and trusses. By neglecting the local effects at the edges and ends, satisfactory solutions can be obtained for many case~. The procedures for reducing the three dimensional equations to two and one dimensional equations are described in Chapter 1, Volume 1, where the various approximations are pointed out |
| Beschreibung: | 1 Online-Ressource (XXXIII, 695 p) |
| ISBN: | 9789400911659 9789401070188 |
| ISSN: | 0924-2139 |
| DOI: | 10.1007/978-94-009-1165-9 |
Internformat
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| 500 | |a The basic partial differential equations for the stresses and displacements in clas sical three dimensional elasticity theory can be set up in three ways: (1) to solve for the displacements first and then the stresses; (2) to solve for the stresses first and then the displacements; and (3) to solve for both stresses and displacements simultaneously. These three methods are identified in the literature as (1) the displacement method, (2) the stress or force method, and (3) the combined or mixed method. Closed form solutions of the partial differential equations with their complicated boundary conditions for any of these three methods have been obtained only in special cases. In order to obtain solutions, various special methods have been developed to determine the stresses and displacements in structures. The equations have been reduced to two and one dimensional forms for plates, beams, and trusses. By neglecting the local effects at the edges and ends, satisfactory solutions can be obtained for many case~. The procedures for reducing the three dimensional equations to two and one dimensional equations are described in Chapter 1, Volume 1, where the various approximations are pointed out | ||
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Datensatz im Suchindex
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| id | DE-604.BV042414961 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T01:20:56Z |
| institution | BVB |
| isbn | 9789400911659 9789401070188 |
| issn | 0924-2139 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027850454 |
| oclc_num | 863860008 |
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| owner_facet | DE-91 DE-BY-TUM DE-83 |
| physical | 1 Online-Ressource (XXXIII, 695 p) |
| psigel | ZDB-2-PHA ZDB-2-BAE ZDB-2-PHA_Archive |
| publishDate | 1989 |
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| series2 | Mechanics of Structural Systems |
| spelling | Gatewood, B. E. Verfasser aut Virtual Principles in Aircraft Structures by B. E. Gatewood Dordrecht Springer Netherlands 1989 1 Online-Ressource (XXXIII, 695 p) txt rdacontent c rdamedia cr rdacarrier Mechanics of Structural Systems 6-7 0924-2139 The basic partial differential equations for the stresses and displacements in clas sical three dimensional elasticity theory can be set up in three ways: (1) to solve for the displacements first and then the stresses; (2) to solve for the stresses first and then the displacements; and (3) to solve for both stresses and displacements simultaneously. These three methods are identified in the literature as (1) the displacement method, (2) the stress or force method, and (3) the combined or mixed method. Closed form solutions of the partial differential equations with their complicated boundary conditions for any of these three methods have been obtained only in special cases. In order to obtain solutions, various special methods have been developed to determine the stresses and displacements in structures. The equations have been reduced to two and one dimensional forms for plates, beams, and trusses. By neglecting the local effects at the edges and ends, satisfactory solutions can be obtained for many case~. The procedures for reducing the three dimensional equations to two and one dimensional equations are described in Chapter 1, Volume 1, where the various approximations are pointed out Engineering Mechanics Mechanical engineering Civil engineering Automotive Engineering Mechanical Engineering Civil Engineering Ingenieurwissenschaften https://doi.org/10.1007/978-94-009-1165-9 Verlag Volltext |
| spellingShingle | Gatewood, B. E. Virtual Principles in Aircraft Structures Engineering Mechanics Mechanical engineering Civil engineering Automotive Engineering Mechanical Engineering Civil Engineering Ingenieurwissenschaften |
| title | Virtual Principles in Aircraft Structures |
| title_auth | Virtual Principles in Aircraft Structures |
| title_exact_search | Virtual Principles in Aircraft Structures |
| title_full | Virtual Principles in Aircraft Structures by B. E. Gatewood |
| title_fullStr | Virtual Principles in Aircraft Structures by B. E. Gatewood |
| title_full_unstemmed | Virtual Principles in Aircraft Structures by B. E. Gatewood |
| title_short | Virtual Principles in Aircraft Structures |
| title_sort | virtual principles in aircraft structures |
| topic | Engineering Mechanics Mechanical engineering Civil engineering Automotive Engineering Mechanical Engineering Civil Engineering Ingenieurwissenschaften |
| topic_facet | Engineering Mechanics Mechanical engineering Civil engineering Automotive Engineering Mechanical Engineering Civil Engineering Ingenieurwissenschaften |
| url | https://doi.org/10.1007/978-94-009-1165-9 |
| work_keys_str_mv | AT gatewoodbe virtualprinciplesinaircraftstructures |