Results 201 to 210 of about 15,386 (232)

Manufacturing of Nano-treated Lower Panel Demonstrators for Aircraft Fuselage

2015
Improved robustness is seen as a key technology enabler for reducing the required thicknesses of composite structural parts; this reduction would, in turn, lead to direct savings in the structural mass. The aim of this study was to produce one reference and two nano-treated lower panel demonstrators for investigating the effect of nano-reinforcement on
Feride Nur Sasal, Aysun Dogangun Akın, Ayhan Kılıc, Guray Erteği, Caglayan Duygu, Emre İşler, Ben Newman, Christos Koimtzoglou, Panagiotis Maroulas, Patrick Bara, Antonios Vavouliotis, George Sotiriadis, Vassilis Kostopoulos   +12 more
openaire   +1 more source

The effect of acoustic-thermal environments on advanced composite fuselage panels

24th Structures, Structural Dynamics and Materials Conference, 1983
Described is a sonic fatigue program to determine the effect of elevated temperature on flat integrally stiffened graphite/epoxy panels. The program involved comparative sonic fatigue testing of two J-stiffened monolithic and two bladed-stiffened orthogrid panels, with one panel of each design tested at ambient temperature and the other at 254°F.
openaire   +1 more source

High-Speed Civil Transport Hybrid Laminate Sandwich Fuselage Panel Test

1999
Hybrid laminates consisting of interspersed titanium foils and carbon fiber-reinforced polymer-matrix composite (PMC) plies are among the leading material candidates for High-Speed Civil Transport (HSCT) primary structure. To demonstrate the feasibility of fabricating large adhesive bonded honeycomb sandwich subcomponents with hybrid laminate ...
M Miller, AC Rufin, WN Westre, G Samavedam   +3 more
openaire   +1 more source

Testing fuselage panels for post-crash fire performance

2011
Aussi disponible en français: Évaluation des produits de combustion dégagés par les matériaux des fuselages d ...
openaire   +1 more source

Experimental Modal Analysis of an Aircraft Fuselage Panel: Part II

Hypersonic aircraft structures must operate in complex loading conditions and very high temperatures, making the design of a robust and reusable platform very challenging. An analytical and experimental test program was developed by the Air Force Research Laboratory (AFRL) and industry.
Travis A. Wyen, Ricardo A. Perez, Jonathan Knox, Joshua J. Schoettelkotte, Thomas G. Eason   +4 more
openaire   +1 more source

Addressing distress management challenges: Recommendations from the consensus panel of the American Psychosocial Oncology Society and the Association of Oncology Social Work

Ca-A Cancer Journal for Clinicians, 2021
Teresa L Deshields, Ryan D Nipp
exaly  

Survival outcomes used to generate version 9 American Joint Committee on Cancer staging system for anal cancer

Ca-A Cancer Journal for Clinicians, 2023
Elliot A Asare
exaly  

Survival outcomes used to validate version 9 of the American Joint Committee on Cancer staging system for appendiceal cancer

Ca-A Cancer Journal for Clinicians, 2023
Elliot A Asare
exaly  

American Cancer Society guideline for diet and physical activity for cancer prevention

Ca-A Cancer Journal for Clinicians, 2020
Cheryl L Rock, Cynthia A Thomson, Ted Gansler   +2 more
exaly  

Development of Glare Fuselage Panels Using a Building Block Approach

2009
5th Joint Canada-Japan Workshop on Composites From 9/6/2004 To 9/8/2004, Yonezawa ...
Poon, C. J., Laliberte, J., Straznicky, P. V., Mendis, Y., Kok, L.   +4 more
openaire   +1 more source