Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Journal of Propulsion Technology》 2005-03
Add to Favorite Get Latest Update

Calculation of the propellant burning rates on the valence electrons fractal combustion model

LIU Jian-hong~1, TIAN De-yu~ 1,2, ZHAO Feng-qi~3, HONG Wei-liang~1, ZHANG Xiao-ping~4, TANG Li-rong~1, ZHENG Jian~4, PANG Ai-min~4(1. Dept.of Chemistry and Biology Normal Coll., Shenzhen Univ., Shenzhen 518060,China; 2.Inst.of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073,China; 3. Xi’an Modern Chemistry Research Inst., Xi’an 710065,China;4.Hubei Inst. of Aerospace Chemotechnology, Xiangfan 410073, China)  
A valence electrons fractal combustion model based on the valence electrons combustion model was proposed. By using fractal dimension to compensate for the surface roughness of the AP, it is possible to deduce some formulas concerned and make computer programming. The Visual Basic NET is used as the programming tool to calculate the burning rates of the composite solid propellants. The results obtained in this model fit with the experimental results better than those in the previous valence electrons combustion model. This demonstrates the new valence electrons fractal combustion model is more reasonable.
【Fund】: 国防科技重点实验室基金项目(51455060101QT5102)。
【CateGory Index】: V512
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved