Isothermal Heat Aging Effects on Mechanical Properties of Carbon/Phenolic Composite Materials for Supersonic Aircrafts

سال انتشار: 1394
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 730

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شناسه ملی سند علمی:

MAARS01_040

تاریخ نمایه سازی: 16 اسفند 1394

چکیده مقاله:

The objective of this paper is to evaluate the effects of isothermal heat aging on the tensile properties of the carbon fiber/phenolic(CFP) composites. Mechanical tests were performed to specimens, which have previously been subjected to the isothermal heat aging conditions. The specimens were exposed to constant temperatures in the range of 150 °C, 200 °C and 250 °C for various periods of times, and then, the residual tensile properties at room temperature were measured. Both the tensile modulus and the ultimate tensile strength of CFP composites decreased with elevated temperatures and these degradations were time and temperature dependent.

نویسندگان

Moslem Najafi

Ph.D. Candidate in Mechanical Engineering Department of Mechanical Engineerin University of Guilan

Seyyed Hamid Mirjani

M.Sc. in Materials Engineering Department of Materials Engineering, Science and Research Branch, Islamic Azad University

Seyyed Mohammad Reza Khalili

Professor of Mechanical Engineering Center of Excellence for Research in Advanced Materials and Structures

Reza Eslami-Farsani

Assistant Professor of Mechanical Engineering Center of Excellence for Research in Advanced Materials and Structures

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  • Swadling S]. Prospects For A Second Geeration Supersonic Transport. Journal ...
  • Regnier N, Guibe C. Methodology for multistage ...
  • 2 _ nvi _ _ _ 1984; 15[1: 25-31. ...
  • http://www. http : / /www. colan.com.au/. ...
  • http : //www. huntsnnan.co, ...
  • Griffiths R, Ball A. A1 assess1nent of the ...
  • fibre composites. Polymer Degradation and Stability 2001; 71: 179-184. ...
  • Halim S, Anmin MB, Maadhah A, Handbook _ New York: ...
  • Mouritz AP, Mathys Z. Post-fire Mechanical Properties of Marine Polymer ...
  • Mouritz AP, Mathys Z. Post-fire Mechanical Properties of Glass-reinfore ed ...
  • Gardiner CP, Mouritz AP, Mathys , Towsed CR. T'ensile and ...
  • Gates T, Grayson _ On the use of ...
  • Inst Aeronaut Astronaut 1998; 2: 925-935. ...
  • Nishimoto W, Nagata آ [13] Sakai W, Sadakane M, Tsutsumi ...
  • Li G, Po urmohamadian N, Cygan A, Peck]. Fast repair ...
  • Grossnnan E, Gouzman I. Space environnment effects on polymers in ...
  • Tsotsis TK, Lee SM. Long-term Therno- oxidative Aging in Composite ...
  • Feih S, Mathys _ Gibson AG, Mouritz AP. T'ensile strength ...
  • Feih S, Mathys Z, Gibson AG, Mouritz AP. Strength degradation ...
  • Adanns DS, Bowles DE, Herakovich CT. ...
  • Chung K, Yoshioka K, seferis]C. ...
  • Fritz W, In: Proceeding of the first seminar onn carbonn ...
  • نمایش کامل مراجع