一種固體火箭發(fā)動(dòng)機(jī)噴管擺動(dòng)冷流縮比試驗(yàn)方法
郭小帆
摘 要：針對(duì)研究噴管擺動(dòng)工況下擴(kuò)壓器工作特性的試驗(yàn)中存在：噴管擺動(dòng)難以實(shí)現(xiàn)；若以高溫高壓蒸汽或者燃?xì)庾鳛橐浣橘|(zhì)，雖引射效率高但耗費(fèi)巨大的人力物力等問(wèn)題在發(fā)動(dòng)機(jī)研制初期很難被采納。該文提出一種以擴(kuò)壓器擺動(dòng)等效噴管擺動(dòng)，以冷空氣作為引射和被引射介質(zhì)的簡(jiǎn)化試驗(yàn)方法。數(shù)值計(jì)算結(jié)果與試驗(yàn)結(jié)果符合較好，試驗(yàn)方法經(jīng)濟(jì)實(shí)用，操作簡(jiǎn)單，可以作為擺動(dòng)噴管固體火箭發(fā)動(dòng)機(jī)研制初期的試驗(yàn)手段。
關(guān)鍵詞：固體火箭發(fā)動(dòng)機(jī)；冷流縮比試驗(yàn)；噴管擺動(dòng)；試驗(yàn)方法
中圖分類號(hào)：V435+.6；TM930.12；V42；V435+.23 文獻(xiàn)標(biāo)志碼：A 文章編號(hào)：1674-5124（2013）05-0039-03
Cold-flow testing of sub-scale model for swinging nozzle of solid-rocket engines
GUO Xiao-fan， YANG Xiao-hui， HE De-sheng， LI Guang-wu
（The 401th Research Institute of the Fourth Academy of CASC，Xi’an 710025，China）
Abstract: There are two questions in the characteristics test of diffuser with the swinging nozzle. Firstly， swinging nozzle is too difficult to achieve. Secondly， although the efficiency of ejector is high in the test which the ejector media is the steam or gas with high temperature and pressure， costly human and material resources are too hard to be adopted in the early development of the solid-rocket motor. To solve problems mentioned above， this paper presented a simplified test method that swinging diffuser is equivalent to swinging nozzle and cold air is used as the ejector media. The numerical results agree well with the available test data. The test method can be applied on the solid-rocket with swinging nozzle principle design because it is convenient， economical and practical.
Key words: solid-rocket engine； cold-flow testing of sub-scale model； swinging nozzle； test method
