导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1997, Vol. 18 ›› Issue (2): 146-152.

Previous Articles     Next Articles

RESIDUAL STRENGTH ESTIMATION OF COMPOSITE LAM INATES WITH DAMAGE

Tang Xiaodong1, Shen Zhen1, Chen Puhui1, Yang Shengchun1, Yang Xu2, Chen Yebiao3   

  1. 1. Aircraft Strength Research Institute, Xi'an, 710065;2. Shenyang Aircraft Design Institute, Shenyang, 110035;3. Chengdu Aircraft Design Institute, Chengdu, 610041
  • Received:1996-02-26 Revised:1996-08-20 Online:1997-04-25 Published:1997-04-25

Abstract:

 A n engineering app roach is developed fo r the residual st rength analysis of damaged,specially impacted, lam inated compo sites. Themain features of the app roach are ① an independent damage characterizat ion method, Damage Data St ructure, DDS, ② a N ew failure criterion ——Damage Influence (D I) criterion fo r no tched specimen, ③ a simp le model, BendingSt rain Energy Density (BSED ) , fo r impact damage p redict ion, ④ an algo rithm of residualst rength analysis fo r single and o rmult ip le delam inat ions, either int roduced by impact o r p reimp lanted. The app licability and effect iveness of th is app roach w ere validated by numerical analysis fo r no tched tension, comp ression of impacted and p reimp lanted delam inat ion, fo r 52 different layup s and of material system s. Good consistency of analysis results w ith test results isobtained.

Key words: laminated composites, damage, strength

CLC Number: