CHENG Cheng, WANG Yibai, LIU Yu, LIN Qingguo. Numerical investigation of low cycle fatigue life for channel wall nozzles[J]. 航空动力学报, 2018, 33(7): 1553-1565.
doi: 10.13224/j.cnki.jasp.2018.07.003
CHENG Cheng, WANG Yibai, LIU Yu, LIN Qingguo. Numerical investigation of low cycle fatigue life for channel wall nozzles[J]. 航空动力学报, 2018, 33(7): 1553-1565.DOI: 10.13224/j.cnki.jasp.2018.07.003.
doi: 10.13224/j.cnki.jasp.2018.07.003DOI:
Numerical investigation of low cycle fatigue life for channel wall nozzles
The thermal-structural response and low cycle fatigue life of a three-dimensional (3D) channel wall nozzle with regenerative cooling were numerically investigated by coupling the finite volume fluid-thermal method
nonlinear finite element thermal-structural analysis and local strain methods. The nozzle had a high area ratio (nozzle exit area divided by throat area) under cyclic working loads. Parametric studies were carried out to evaluate the effects of channel structural parameters such as channel width
channel height
liner thickness and rib width. Results showed that the integrated effects of three-dimensional channel structure and load distribution caused serious strain
which mainly occurred at the intersectant regions of liner wall on the gas side and the symmetric planes of channel and rib. The cooling effect and channel structural strength were significantly improved as the channel width and height decreased
leading to substantial extension of the nozzle service life. On the other hand
the successive decrease in liner thickness and rib width apparently increased the strain amplitude and residual strain of channel wall nozzle during cyclic work
significantly shortening the service life. The present work is of value for design of the channel wall nozzle to prolong its cyclic service life.
Abstract
The spontaneous ignition performances of a cavity-based strut flameholder were preliminarily investigated with spray distances of 5-50mm at atmospheric pressure
the air temperature and oxygen volume fraction were within the range of 750-900℃ and 13.4%-15.8%
Mach number ranged from 0.20-0.28. Results showed that the flameholder could be autoignited when the inlet temperature was above 850℃. As the inlet temperature increased
the performances of spontaneous ignition improved. When the inlet Mach number became larger
the temperature range for successful spontaneous ignition became narrower. With the increase of fuel injection distance
the autoignition performances of the stabilizer were improved. The cavity structure of the stabilizer could stabilize the flame.