scholarly journals Deflagration-to-Detonation Transition in Nitrous Oxide-Ethylene Mixtures and its Application to Pulsed Propulsion Systems

2017 ◽  
Author(s):  
Prashanth Bangalore Venkatesh ◽  
Tyler Graziano ◽  
Sally P. Bane ◽  
Scott Meyer ◽  
Mark C. Grubelich
Keyword(s):  
Nitrous Oxide ◽  
Propulsion Systems ◽  
Deflagration To Detonation Transition ◽  
Detonation Transition

scholarly journals The Principal Aspects of Application of Detonation in Propulsion Systems

2013 ◽  
Vol 2013 ◽  
pp. 1-15 ◽  
Author(s):  
A. A. Vasil'ev
Keyword(s):  
Supersonic Flow ◽  
Combustible Mixture ◽  
Experimental Results ◽  
Detonation Waves ◽  
Propulsion Systems ◽  
Air Breathing ◽  
Deflagration To Detonation Transition ◽  
Detonation Engine ◽  
Detonation Process ◽  
Detonation Transition

The basic problems of application of detonation process in propulsion systems with impulse and continuous burning of combustible mixture are discussed. The results on propagation of detonation waves in supersonic flow are analyzed relatively to air-breathing engine. The experimental results are presented showing the basic possibility of creation of an engine with exterior detonation burning. The base results on optimization of initiation in impulse detonation engine are explained at the expense of spatial and temporal redistribution of an energy, entered into a mixture. The method and technique for construction of highly effective accelerators for deflagration to detonation transition are discussed also.

scholarly journals Deflagration-to-Detonation Transition in Nitrous Oxide/Oxygen-Fuel Mixtures for Propulsion

2019 ◽  
Vol 35 (5) ◽  
pp. 944-952 ◽  
Author(s):  
Prashanth Bangalore Venkatesh ◽  
Scott E. Meyer ◽  
Sally P. M. Bane ◽  
Mark C. Grubelich
Keyword(s):  
Nitrous Oxide ◽  
Deflagration To Detonation Transition ◽  
Nitrous Oxide Oxygen ◽  
Detonation Transition ◽  
Fuel Mixtures ◽  
Oxygen Fuel

RANKING OF FUEL-AIR MIXTURES IN TERMS OF THEIR PROPENSITYTO DEFLAGRATION-TO-DETONATION TRANSITION

2020 ◽  
Author(s):  
S. M. FROLOV ◽  
◽  
V. I. ZVEGINTSEV ◽  
V. S. AKSENOV ◽  
I. V. BILERA ◽  
...  
Keyword(s):  
Detonation Wave ◽  
The Other ◽  
Practical Application ◽  
Deflagration To Detonation Transition ◽  
Other Hand ◽  
Pressure Gain Combustion ◽  
Reactive Mixture ◽  
Detonation Transition ◽  
The One ◽  
Energy Converting

The term "detonability" with respect to fuel-air mixtures (FAMs) implies the ability of a reactive mixture of a given composition to support the propagation of a stationary detonation wave in various thermodynamic and gasdynamic conditions. The detonability of FAMs, on the one hand, determines their explosion hazards during storage, transportation, and use in various sectors of the economy and, on the other hand, the possibility of their practical application in advanced energy-converting devices operating on detonative pressure gain combustion.

DEFLAGRATION-TO-DETONATION TRANSITION IN A STRATIFIED SYSTEM “GASEOUS OXYGEN-LIQUID FILM OF N-DECANE”

2020 ◽  
Author(s):  
S. M. FROLOV ◽  
◽  
V. S. AKSENOV ◽  
I. O. SHAMSHIN ◽  
◽  
...  
Keyword(s):  
Liquid Film ◽  
Ignition Source ◽  
Gaseous Oxygen ◽  
Deflagration To Detonation Transition ◽  
Operation Process ◽  
Continuous Detonation ◽  
Smooth Channel ◽  
Detonation Transition ◽  
Run Up ◽  
X 24

Deflagration-to-detonation transition (DDT) in the system “gaseous oxygen- liquid film of n-decane” ' with a weak ignition source was obtained experimentally. In a series of experiments with ignition by an exploding wire that generates a weak primary shock wave (SW) with a Mach number ranging from 1.03 to 1.4, the DDT with the detonation run-up distances 1 to 4 m from the ignition source and run-up time 3 ms to 1.7 s after ignition was observed in a straight smooth channel of rectangular 54 x 24-millimeter cross section, 3 and 6 m in length with one open end. The DDT is obtained for relatively thick films with a thickness of 0. 3-0.5 mm, which corresponds to very high values of the overall fuel-to-oxygen equivalence ratios of 20-40. The registered velocity of the detonation wave (DW) was 1400-1700 m/s. In a number of experiments, a high-velocity quasi-stationary detonation-like combustion front was recorded running at an average velocity of 700-1100 m/s. Its structure includes the leading SW followed by the reaction zone with a time delay of 90 to 190 s. The obtained results are important for the organization of the operation process in advanced continuous-detonation and pulsed-detonation combustors of rocket and air-breathing engines with the supply of liquid fuel in the form of a wall film.

Flame Speed and Deflagration-Detonation Analysis in Flare Stack and Header

2018 ◽  
Author(s):  
Philip Diwakar ◽  
Jaleel Valappil
Keyword(s):  
Ambient Air ◽  
Flame Speed ◽  
Safety Concerns ◽  
Deflagration To Detonation Transition ◽  
Detonation Transition

This paper examines safety concerns related to flame speeds when warm relief gas snuffs out the pilot at the flare stack and pulls in ambient air and a spark ignites the vapor in the header. The flame speed essentially determines if the propagating flame speed is a deflagration or a detonation based on whether its subsonic or supersonic. While pipes are sized for deflagrations, they need to be analyzed and tested for detonation pressures and temperatures. Transient CFD calculations help determine the flame speeds, deflagration to detonation transition, pressures and temperatures are compared to pipe specifications and help determine if a detonation leads to a Loss of Containment and suggests mitigations.

scholarly journals Heating of the fuel mixture due to viscous stress ahead of accelerating flames in deflagration-to-detonation transition

2008 ◽  
Vol 372 (27-28) ◽  
pp. 4850-4857 ◽  
Author(s):  
Damir Valiev ◽  
Vitaly Bychkov ◽  
V'yacheslav Akkerman ◽  
Lars-Erik Eriksson ◽  
Mattias Marklund
Keyword(s):  
Fuel Mixture ◽  
Viscous Stress ◽  
Deflagration To Detonation Transition ◽  
Detonation Transition

Deflagration-to-Detonation Transition of Methane-Oxygen Mixtures in Narrow Tubes

2015 ◽  
pp. 295-300
Author(s):  
V. V. Golub ◽  
S. V. Golovastov ◽  
K. V. Ivanov ◽  
D. I. Baklanov ◽  
D. A. Lenkevich ◽  
...  
Keyword(s):  
Deflagration To Detonation Transition ◽  
Detonation Transition
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