PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Tension field in thin-walled aeronautical girders

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper describes the influence of the field of draws on the state of effort of thin-walled girders, particularly on the state of burdening elements of connections of metal sheets of web of an I-beam with elements of the framework, e.g.: of riveted joints appearing in structures of this type. In the paper were presented results of analyses of girders without and with lightening holes. A fact brought up in this paper, is that implementing lightening holes is raising the critical strength of covering but an also causes increase of normal stresses appearing in elements of the skeleton and of shear stresses in connections.
Rocznik
Strony
291--308
Opis fizyczny
Bibliogr. 14 poz.
Twórcy
autor
autor
  • Instytut Podstaw Budowy Maszyn, Technical University of Warsaw, Narbutta 84, 02-524 Warsaw, Poland
Bibliografia
  • [1] ABAQUS Analysis User's Manual, ABAQUS, Inc. United States of America, 2004.
  • [2] Brzoska, Z. Statics and stability of the rod and thin-walled structures, Warsaw, National Scientific; Publishers, 1961.
  • [3] Brzoska, Z. Statics and stability of the rod and thin walled structures, Second Edition - amended, Warsaw, National Scientific Publishers, 1965.
  • [4] Hertel, H. Leichtbau Flugzeuge Und Andere Leichtbullwerke, Springer- Verlag, Berlin / Gottingen / Heidelberg, 1960.
  • [5] Jachimowicz, J. Static analysis of rigidity-strength machine housings, Dissertation, Warsaw University of Technology, 1995.
  • [6] Ko, W.L. and Jackson, R.H. Shear buckling analysis of a hat-stiffened panel, Edwards, California: NASA Dryden Flight Research Center, Technical Memorandum, NASA-TM-4644, 1994.
  • [7] Kuhn, P. Stresses In Aircraft and Shell Structures, McGraw-Hill Book Company Inc., New York / Toronto / Londyn, 1956.
  • [8] Payload Flight Equipment Requirements and Guidelines for Safety-Critical Structures, National Aeronautics and Space Administration, International- Space Station Program, Johnson Space Center, Houston, Teras, Contract No. NAS9-02099 (PA16), 2002.
  • [9] Simon, H. and Wagner, H. Über die Krafteinleitung in Dunnwandige Zylinderschalen, Luftfahrtforschung, vol. 13, No. 9, 1936.
  • [10] Teisseyre, J. Construction of bodies. Part I - calculation, Warsaw, Transport and Communication Publishers, 1965.
  • [11] Tessler, A., Sleight, D.W. and Wang, J.T. Nonlinear shell modeling of thin membranes with emphasis on structural wrinkling, Hampton. NASA Langley Research Center, Analytical and Computational Methods Branch, Structures and Materials Competency, VA 23681-2199, 2003.
  • [12] Tessler, A., Sleight, D.W. and Wang, J.T. Nonlinear shell modeling of thin membranes with emphasis on structural wrinkling, Hampton: NASA Langley Research Center, Analytical and Computational Methods Branch, Structures and Materials Competency, VA 23681-2199, 2003.
  • [13] Wang,J.T., Chen T., Sleight, D.W. and Tessler, A. Simulating non-linear deformations of solar sail membranes using explicit time integration, Palm Springs, California: NASA Langley Research Center, Hampton, 45th AIAA/ ASME/ ASCE/ AHS / ASC Structures, Structural Dynamics and Materials Conference, VA 23681-2199, 2004.
  • [14] PN-84/H-93669, Aluminum and aluminum alloys. Profiles.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD9-0027-0021
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.