空气动力学学报
空氣動力學學報
공기동역학학보
ACTA AERODYNAMICA SINICA
2009年
z1期
21-28
,共8页
朱雨建%杨基明%韩肇元%J.H.S.Lee
硃雨建%楊基明%韓肇元%J.H.S.Lee
주우건%양기명%한조원%J.H.S.Lee
爆轰%激波%迎面撞击%扫描纹影
爆轟%激波%迎麵撞擊%掃描紋影
폭굉%격파%영면당격%소묘문영
detonation%shock%head - on collision%streak schlieren
本文为对当量比乙炔氧气混合气体中爆轰波与激波正面对撞产生稳定波系的实验和理论研究.实验主要以高速扫描摄影获取两波对撞的x-t纹影图,一维理论分析则基于三种热完全的组分求解两波对撞的稳定解并探寻它们的规律.实验发现透射波系包括一道激波和爆轰波,以及紧随爆轰波后的稀疏波区,这种波系情况与一维理论分析中CJ解一致.透射CJ爆轰与人射爆轰相比马赫数降低,而相对波前来流的传播速度有轻微提高,但在实验室坐标下其速度显著降低.透射波系受初始压强影响不大;初始温度提高使得爆轰波速度降低,而透射激波速度增加;对波系起实质影响作用的是入射激波强度,激波越强,则整个透射流场呈现偏向激波的趋势;理论分析还指出,稀疏波区的出现不可避免,当激波强度趋于声波时稀疏波区趋于消失,激波越强则疏波区趋于扩大.
本文為對噹量比乙炔氧氣混閤氣體中爆轟波與激波正麵對撞產生穩定波繫的實驗和理論研究.實驗主要以高速掃描攝影穫取兩波對撞的x-t紋影圖,一維理論分析則基于三種熱完全的組分求解兩波對撞的穩定解併探尋它們的規律.實驗髮現透射波繫包括一道激波和爆轟波,以及緊隨爆轟波後的稀疏波區,這種波繫情況與一維理論分析中CJ解一緻.透射CJ爆轟與人射爆轟相比馬赫數降低,而相對波前來流的傳播速度有輕微提高,但在實驗室坐標下其速度顯著降低.透射波繫受初始壓彊影響不大;初始溫度提高使得爆轟波速度降低,而透射激波速度增加;對波繫起實質影響作用的是入射激波彊度,激波越彊,則整箇透射流場呈現偏嚮激波的趨勢;理論分析還指齣,稀疏波區的齣現不可避免,噹激波彊度趨于聲波時稀疏波區趨于消失,激波越彊則疏波區趨于擴大.
본문위대당량비을결양기혼합기체중폭굉파여격파정면대당산생은정파계적실험화이론연구.실험주요이고속소묘섭영획취량파대당적x-t문영도,일유이론분석칙기우삼충열완전적조분구해량파대당적은정해병탐심타문적규률.실험발현투사파계포괄일도격파화폭굉파,이급긴수폭굉파후적희소파구,저충파계정황여일유이론분석중CJ해일치.투사CJ폭굉여인사폭굉상비마혁수강저,이상대파전래류적전파속도유경미제고,단재실험실좌표하기속도현저강저.투사파계수초시압강영향불대;초시온도제고사득폭굉파속도강저,이투사격파속도증가;대파계기실질영향작용적시입사격파강도,격파월강,칙정개투사류장정현편향격파적추세;이론분석환지출,희소파구적출현불가피면,당격파강도추우성파시희소파구추우소실,격파월강칙소파구추우확대.
An experimental and theoretical study on the steady wave system after head - on collision of a detonation wave with shock wave was carried out. Experimentally, high speed streak sehlieren photography was used to illustrate the interacting flow field. And theoretically, 1 - dimensional analytic works based on 3 combined species were also performed to find the steady solution of the collision problem and its essential characteristics. The x - t streak schlieren photos demonstrate that the steady wave system after collision consists of a shock wave and a detonation wave followed by a rarefaction wave fan, and this result is consistent with the CJ solution of 1 - D theoretical analysis. By the impact of incident shock, the Mach number of transmitted detonation decreases, while the propagation speed of it relative to the flow ahead is slightly increased and in laboratory frame it shows up to be decreased due to the shockinduced opposite flow. The wave system is barely depending on the initial pressure of the mixture, while initial temperature can remarkably decrease detonation speeds and increase transmitted shock speed. The strength of the incident shock wave serves as the most important parameter that controls the transmitted flow system. Stronger shock pulls the whole flow field towards the shock direction more seriously. Rarefaction is inevitable in the system unless the incident shock tends to Mach one, and stronger shock usually results in more expanded rarefaction zone.