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1.
In this study, detonation cell sizes of methanol–oxygen mixtures are experimentally measured at different initial pressures
and compositions. Good agreement is found between the experiment data and predictions based on the chemical length scales
obtained from a detailed chemical kinetic model. To assess the detonation sensitivity in methanol–oxygen mixtures, the results
are compared with those of hydrogen–oxygen and methane–oxygen mixtures. Based on the cell size comparison, it is shown that
methanol–oxygen is more detonation sensitive than methane–oxygen but less sensitive than hydrogen–oxygen. 相似文献
2.
Yu. N. Belyaev 《Journal of Applied Mechanics and Technical Physics》1995,36(1):60-66
Moscow. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 1, pp. 64–72, January–February, 1995. 相似文献
3.
I. V. Sturova 《Journal of Applied Mechanics and Technical Physics》1994,35(5):670-679
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 5, pp. 32–44, Septerm–October, 1994. 相似文献
4.
H. R. Pakzad 《Shock Waves》2011,21(4):357-365
Dust acoustic shock waves of the Korteweg-de Vries–Burgers (KdV–Burgers) equation and the modified Korteweg-de Vries–Burgers
(MKdV–Burgers) equation are studied in strongly coupled dusty plasmas containing nonthermal ions and Boltzmann-distributed
electrons. The effects of important parameters, such as nonthermal parameter, relative temperature, relative density and dust
particles viscosity, on the properties of shock waves are discussed. 相似文献
5.
L. P. Gorbachev S. V. Novikov V. B. Sokolov V. F. Fedorov Yu. A. Frolov P. O. Shishkov 《Journal of Applied Mechanics and Technical Physics》1995,36(1):1-3
Moscow. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 1, pp. 3–5, January–February, 1995 相似文献
6.
David E. Zeitoun Yves Burtschell Irina A. Graur Mikhail S. Ivanov Alexey N. Kudryavtsev Yevgeny A. Bondar 《Shock Waves》2009,19(4):307-316
Numerical simulations of shock wave propagation in microchannels and microtubes (viscous shock tube problem) have been performed
using three different approaches: the Navier–Stokes equations with the velocity slip and temperature jump boundary conditions,
the statistical Direct Simulation Monte Carlo method for the Boltzmann equation, and the model kinetic Bhatnagar–Gross–Krook
equation with the Shakhov equilibrium distribution function. Effects of flow rarefaction and dissipation are investigated
and the results obtained with different approaches are compared. A parametric study of the problem for different Knudsen numbers
and initial shock strengths is carried out using the Navier–Stokes computations.
相似文献
7.
Yu. A. Bogan 《Journal of Applied Mechanics and Technical Physics》1994,35(3):476-480
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 3, pp. 168–173, May–June, 1994. 相似文献
8.
Yu. P. Zakharov O. M. Orishich V. N. Snytnikov I. F. Shaikhislamov 《Journal of Applied Mechanics and Technical Physics》1994,35(3):481-486
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 3, pp. 174–180, May–June, 1994. 相似文献
9.
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 6, pp. 63–69, November–December, 1994. 相似文献
10.
V. L. Khitrik 《Journal of Applied Mechanics and Technical Physics》1994,35(4):556-562
Sergiev Posad, Moscow Oblast. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 4, pp. 78–85. July–August,
1994. 相似文献
11.
S. V. Kuz'min V. I. Lysak D. V. Starikov 《Journal of Applied Mechanics and Technical Physics》1994,35(5):805-807
Volgograd. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 5, pp. 173–175, September–October, 1994 相似文献
12.
V. M. Sadovskii 《Journal of Applied Mechanics and Technical Physics》1994,35(5):798-804
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 5, pp. 166–172, September–October, 1994. 相似文献
13.
V. G. Chernyak I. V. Chermyaninov E. A. Vilisova E. A. Subbotin 《Journal of Applied Mechanics and Technical Physics》1994,35(5):643-652
Ekaterinburg. Translated from Prikladaya Mekhanika i Tekhnicheskaya Fizika, No. 5, pp. 3–13, September–October, 1994. 相似文献
14.
I. A. Banshchikova I. Yu. Tsvelodub 《Journal of Applied Mechanics and Technical Physics》1996,37(6):876-883
Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 37, No. 6, pp. 122–131, November–December, 1996. 相似文献
15.
A. A. Charakhch'yan 《Journal of Applied Mechanics and Technical Physics》1994,35(4):506-514
Moscow. Translated from Prikladnaya Mekhanika i Technicheskaya Fizika, No. 4, pp. 22–32, July–August 1994. 相似文献
16.
Kevin Zumbrun 《Archive for Rational Mechanics and Analysis》2011,200(1):141-182
Confirming a conjecture of Lyng–Raoofi–Texier–Zumbrun, we show that stability of strong detonation waves in the ZND, or small-viscosity,
limit is equivalent to stability of the limiting ZND detonation together with stability of the viscous profile associated
with the component Neumann shock. Moreover, on bounded frequencies the nonstable eigenvalues of the viscous detonation wave
converge to those of the limiting ZND detonation, while on frequencies of order one over viscosity, they converge to one over
viscosity times those of the associated viscous Neumann shock. This yields immediately a number of examples of instability
and Hopf bifurcation of reacting Navier–Stokes detonations through the extensive numerical studies of ZND stability in the
detonation literature. 相似文献
17.
A. G. Kotousov 《Journal of Applied Mechanics and Technical Physics》1994,35(2):274-278
Moscow. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 2, pp. 118–123, March–April, 1994. 相似文献
18.
G. I. Kulakov G. E. Yakovitskaya 《Journal of Applied Mechanics and Technical Physics》1994,35(5):793-797
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 5, pp. 160–165, September–October, 1994. 相似文献
19.
V. Ya. Kiselev A. A. Maslov A. N. Shiplyuk 《Journal of Applied Mechanics and Technical Physics》1994,35(2):224-227
Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 2, pp. 66–69, March–April, 1994. 相似文献
20.
The propagation mechanism of high speed turbulent deflagrations 总被引:2,自引:0,他引:2
The propagation regimes of combustion waves in a 30 cm by 30 cm square cross–sectioned tube with an obstacle array of staggered
vertical cylindrical rods (with BR=0.41 and BR=0.19) are investigated. Mixtures of hydrogen, ethylene, propane, and methane with air at ambient conditions over a range
of equivalence ratios are used. In contrast to the previous results obtained in circular cross–sectioned tubes, it is found
that only the quasi–detonation regime and the slow turbulent deflagration regimes are observed for ethylene–air and for propane–air.
The transition from the quasi–detonation regime to the slow turbulent deflagration regime occurs at (where D is the tube “diameter” and is the detonation cell size). When , the quasi–detonation velocities that are observed are similar to those in unobstructed smooth tubes. For hydrogen–air mixtures,
it is found that there is a gradual transition from the quasi–detonation regime to the high speed turbulent deflagration regime.
The high speed turbulent deflagration regime is also observed for methane–air mixtures near stoichiometric composition. This
regime was previously interpreted as the “choking” regime in circular tubes with orifice plate obstacles. Presently, it is
proposed that the propagation mechanism of these high speed turbulent deflagrations is similar to that of Chapman–Jouguet
detonations and quasi-detonations. As well, it is observed that there exists unstable flame propagation at the lean limit
where . The local velocity fluctuates significantly about an averaged velocity for hydrogen–air, ethylene–air, and propane–air mixtures.
Unstable flame propagation is also observed for the entire range of high speed turbulent deflagrations in methane–air mixtures.
It is proposed that these fluctuations are due to quenching of the combustion front due to turbulent mixing. Quenched pockets
of unburned reactants are swept downstream, and the subsequent explosion serves to overdrive the combustion front. The present
study indicates that the dependence on the propagation mechanisms on obstacle geometry can be exploited to elucidate the different
complex mechanisms of supersonic combustion waves.
Received 5 November 2001 / Accepted 12 June 2002 / Published online 4 November 2002
Correspondence to: J. Chao (e-mail: jenny.chao@mail.mcgill.ca)
An abridged version of this paper was presented at the 18th Int. Colloquium on the Dynamics of Explosions and Reactive Systems
at Seattle, USA, from July 29 to August 3, 2001. 相似文献