您要查找的是不是:
- Possibly due to the left unreacted or partly reacted mixture behind gaseous detonation wave, the reflected shock accelerates at low initial pressure more than at high initial pressure. 在低初压下,可能还由于爆轰彼后未反应或部分反应气体的作用,导致反射激波加速幅度比高初压下大。
- Analysis of Flow Field after Gaseous Detonation Wave is Mach Reflected on an Obstacle 气相爆轰波在障碍物上Mach反射后流场的分析
- Numerical Simulation of Gaseous Detonation Wave Propagation Through Bends with a Detailed Chemical Reaction Model 爆轰波在弯管内传播过程数值分析
- The Experimental Study of Strength Attenuation of Gaseous Detonation Wave Through Acoustic Absorbing Walled Channel 气相爆轰波通过声学吸收壁时强度衰减过程的实验研究
- Study on acceleration of shock generated by normal reflection of gaseous detonation wave 气相爆轰波正反射激波加速研究
- gaseous detonation wave 气相爆轰波
- The Experimental Evidence for Mach Reflection of Gaseous Detonation Waves Acting on an Obstacle 气相爆轰波在障碍物上Mach反射的实验验证
- Numerical Simulation of Cellar Structures and Mach Reflection of Gaseous Detonation Waves 气相爆轰胞格结构和马赫反射数值模拟
- Gaseous detonation propagation through a bifurcated tube was numerically investigated. 摘要数值研究气相爆轰波在分叉管中的传播现象。
- The re-initiation phenomenon of gaseous detonation induced by shock reflection in a bifurcated tube was studied. 摘要以分叉管为例,研究了激波反射诱导气相爆轰二次起爆的现象。
- The re-initiation phenomenon of gaseous detonation in a heart-shape tube was numerically studied. 针对心形管内气相爆轰二次起爆过程进行了数值研究。
- Propagation characteristics of unsteady gaseous detonation in propane? oxygen? air mixtures through90° bend were studied by experiments. 对丙烷-氧气-空气的混合气体非稳定爆轰波通过90°弯管传播特性的变化进行了初步的实验研究.
- After gaseous detonation reflects on the right wall, the right-traveling rarefaction waves accelerate the reflected shock. 气相爆轰波在右壁面反射后,右行稀疏波加速反射激波。
- The computed evolution of detonation wave involving the re-initiation is in good agreement with the schlieren images. 计算得到的二次起爆过程波系演变与实验纹影照片基本一致。
- An experimental investigation is presented concerning the re-intension process of a detonation wave occurring downstream of the acoustic absorbing walled section in this paper. 摘要实验研究了爆轰波在声学吸收段下游发生的再恢复过程。
- According to the method of DSD, we used analytical method to acquire the steady state developed equation of detonation wave. 并根据DSD方法,结合实验所得炸药爆轰波波形,通过解析的方法求得炸药爆轰波阵面在拟定态时的发展方程。
- The unsteady blowdown process after the CJ detonation wave reach the exit of detonation tube was two-dimensional axisymmetric numerical simulated. 对爆震波到达爆震管口后,发动机的非定常排气过程进行了二维轴对称数值模拟。
- Then a building up detonation wave propagates throughout the heterogeneous explosive charge until it develops into a normal detonation. 经过若干微秒的感应时间后,爆轰波在前端面处产生,并开始追赶初始冲击波。
- Method of characteristic (MOC) was used to calculate one-dimensional CJ (Chapman-Jouguet) detonation wave propagating in the ideal detonation tube. 应用特征线法给出一维CJ爆震波在理想爆震管内传播过程的解析解。
- The DDT distance would he lengthened when the gap between the cone and plate was increased, but the pressure of detonation wave was influenced little by the reflector. 而反射锥与反射孔板的间跟增大,爆震波形成距离增大,一旦形成稳定的爆震波后,反射器对爆震波压力的影响不大。