Structural Stability of a Stiffened Aluminum Fuselage Panel Subjected to Combined Mechanical And Internal Pressure-Reference-Cited by-同舟云学术

Structural Stability of a Stiffened Aluminum Fuselage Panel Subjected to Combined Mechanical And Internal Pressure

Published:2003-04-07 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Rouse Marshall,Young Richard,Gehrki Ralph

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1423

Reference4 articles.

1. M.J. "FacilitiesforCombined Loads Testing of AircraftStructurestoSatisfyStructuralTechnology Development Requirements," presentedatthe5th Annual Advanced CompositesTechnology Conference,Seattle, WA,August 22-36,1994. 3. Ambur,D.R., Cerro, J. A., and Dickson, J. D. "D

2. Box Fixture for Testing Stiffened Panels in CompressionandPressure,"JournalofAircraft,Vol.32, No. 6,Nov.Dec. 1995,pp.1382-1389. 4. Anon.PATRAN Plus User Manual - Release3.0,

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical and experimental investigation of a metallic fuselage stiffened panel loaded with a representative fuselage fatigue spectrum;International Journal of Fatigue;2024-05

2. Numerical Investigation of an Experimental Setup for Thermoplastic Fuselage Panel Testing in Combined Loading;Aerospace;2024-02-22

3. Testing Structural Elements under Multiaxial Loading: A Numerical Model of the Bench to Understand and Predict Complex Boundary Conditions;Aerospace;2024-01-10

4. Design and development of an experimental bench concept for testing of fuselage stiffened panels, using a virtual testing methodology;Aircraft Engineering and Aerospace Technology;2023-11-08

5. Experimental behaviour of aeronautical notched carbon fibre reinforced thermoplastic panels under combined tension-shear-pressure loadings;Engineering Failure Analysis;2023-04