固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2008年
2期
173-178
,共6页
固体火箭发动机%封头%屈曲分析
固體火箭髮動機%封頭%屈麯分析
고체화전발동궤%봉두%굴곡분석
solid rocket motor%dome%buckling analysis
用ANSYS软件对固体发动机壳体后封头进行了外压屈曲分析.结果表明,在可承受相同内压条件下金属壳体后封头比复合材料壳体后封头有更高的承受外压能力;壳体后接头、喷管固定体对后封头承外压能力有加强作用;壳体后开口直径越大,临界屈曲载荷越大.
用ANSYS軟件對固體髮動機殼體後封頭進行瞭外壓屈麯分析.結果錶明,在可承受相同內壓條件下金屬殼體後封頭比複閤材料殼體後封頭有更高的承受外壓能力;殼體後接頭、噴管固定體對後封頭承外壓能力有加彊作用;殼體後開口直徑越大,臨界屈麯載荷越大.
용ANSYS연건대고체발동궤각체후봉두진행료외압굴곡분석.결과표명,재가승수상동내압조건하금속각체후봉두비복합재료각체후봉두유경고적승수외압능력;각체후접두、분관고정체대후봉두승외압능력유가강작용;각체후개구직경월대,림계굴곡재하월대.
Buckling analysis on rear dome of solid rocket motor case was studied by means of ANSYS.Results show that the rear dome of metal case can support higher pressure than that of composite case under the same internal pressure.The case rear joint and the fixed body of the nozzle can reinforce the case rear dome obviously.Furthermore,the larger diameter of case rear aperture is,the greater critical buckling load of case rear dome is.