Shock-compressed Gas Research Articles

Transition of convective combustion of solid fuels into weak detonation

The rate of layer-by-layer combustion of a monolithic solid unitary fuel is relatively slow, and depending on the external conditions equals -lO-S-lO "~ m/seco The mechanism of [lame propagation from layer to layer is determined by heat conduction in the condensed phase. In porous fuels, in the presence of longitudinal cracks and channels with small diameter, the velocity of propagation of the flame for separate compositions equals -10=-10 3 m/sec. In this case, the mechanism of flame propagation is qualitatively different: inflammation of subsequent layers is determined by convecti~a heat transfer as a result of leakage of hot reaction products into the channel. Depending on the composition of the fuel and the dimensions of the channel different mechanisms of propagation of convective combustion are possible. For relatively low rates of leakage into the channel the walls ignite as a result of direct contact with the hot reaction products; for high rates of leakage into the channel a shockwave (SW) forms, whose intensity is high enough for the flow of shock compressed gas to ignite directly the surface of the channel.

Thermal action of shock-compressed gas on the surface of colliding plates

Thermal action of shock-compressed gas on the surface of colliding plates

Observations of the shock in a region of shock-induced star formation - NGC 281

view Abstract Citations (23) References (15) Co-Reads Similar Papers Volume Content Graphics Metrics Export Citation NASA/ADS Observations of the shock in a region of shock-induced star formation: NGC 281. Elmegreen, B. G. ; Moran, J. M. Abstract Evidence for the cooled postshock layer situated between the expanding H II region NGC 281 and an adjacent molecular cloud is shown by a well-sampled map of (C-12)O and (C-13)O line profiles having 0.16-km/s resolution. The shocked region shows a higher (C-12)O temperature and column density than the unshocked cloud, and the shock velocity is 1.5 to 2 km/s, depending on position. An H2O maser located at the site of peak shock activity was observed at three epochs separated by 4.5 and 10 months, respectively. The H2O line velocities and strengths show considerable variation, but the strongest emission line is always within + or - 1 km/s of the neutral cloud velocities. It is suggested that the associated maser source is a middle- to late-type B star that was formed in the shock-compressed gas. Publication: The Astrophysical Journal Pub Date: January 1979 DOI: 10.1086/182874 Bibcode: 1979ApJ...227L..93E Keywords: B Stars; Compressed Gas; Shock Waves; Star Formation; Water Masers; Carbon Monoxide; H Ii Regions; Line Spectra; Propagation Velocity; Radio Emission; Astrophysics; Interstellar Matter:Star Formation; Shock Waves:Star Formation; Star Formation:Water Masers full text sources ADS |

Propagation of a shock wave in a channel when shock-compressed gas interacts with a nonhomogeneous magnetic field: PMM vol. 34, n≗4, 1970, pp. 672–684

Propagation of a shock wave in a channel when shock-compressed gas interacts with a nonhomogeneous magnetic field: PMM vol. 34, n≗4, 1970, pp. 672–684

Nonstationary phenomena in gaseous detonation

Recent progress in the shock-tube study of ignition kinetics in various detonable gases can be now utilized for the interpretation of gasdynamic phenomena associated with the detonation process. As a consequence of current knowledge of these processes, globally stationary multiwave detonations must be considered as intimately associated with such essentially nonstationary flow phenomena as those occurring in the course of the transition to detonation or in the decoupling and re-establishment of the detonation wave that takes place close to the limits of detonability. In particular, the following features have come to light: 1. Ignition kinetics associated with the transition to detonation should be considered under the transient gasdynamic processes, and this must include, the effects of positive temperature and density gradients in the flow field. While the induction time can be “accumulated” in a simple compression wave, in a shock-heated gas an “explosion in explosion” may develop leading to the establishment of a detonation wave. More detailed gasdynamic analysis based on concrete kinetics may explain the difference in the length of “induction distances” observed in various experiments. Similar type of phenomena can be observed when the detonation wave is initiated by incident or reflected waves in shock tubes. 2. Blast waves or diffracting detonation waves in a combustible mixture produce negative gradients in the temperature and density behind the shock front. Even in quite strong waves, with parameters close to the CJ condition, the ignition zone becomes decoupled from the shock front and a local, secondary self-ignition may occur in the shock-compressed gas, leading to the re-establishment of detonation. The multilocus ignition mechanism observed in shock-tube experiments can be used to explain some of these observations. On the basis of ignition kinetics in the transient flow field of a diverging shock front, as it occurs in a decoupled wave, the following estimate of the wave thickness can be derived: τ (ind)≅ (d/dr)τ(ρ, T)rτ (ind), where r is the characteristic thickness of the reaction zone behind the diverging shock front. According to this estimate, the spacing of the wave (i.e., the shock wave radius) should be of the order of 10 r , depending on the value of the activation energy in the rate-controlling reaction. 3. Gasdynamic processes that take place in a multihead detonation front are then explained in relation to both the topics described above. Transverse wave collisions lead periodically to fast explosions of small samples of the compressed gas in the reaction zone, producing a number of nonstationary expanding blast waves. Decoupling processes in these waves can be described in the same terms as those used for divering waves, and an average spacing of transverse waves in a stationary multifront wave can be evaluated. Depending on kinetic parameters of the ignition reactions, a “hydrodynamic” thickness of the multiheaded front may be of about 1 order of magnitude larger than the thickness of a reasonable induction reaction zone in a planar one-dimensional detonation wave. On this basis, recent results of different research groups concerned with the study of the detonation wave structure are discussed.