Astronomy & Space Sciences
Title: | Deflagration-to-Detonation Transition Studies in a Detonation Tube Facility |
Area: | Astronomy & Space Sciences |
Focus Area: | Aerospace Engineering |
Status: | Under Development |
Social Benefits: | The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society. |
Developing Agency: | Indian Institute of Technology (IIT) Kanpur, Uttar Pradesh |
Source Title: | Indian Space Research Organisation (ISRO)- Department of Space (DOS) 2022-2024 |
Brief Description
Description : | The aim of the study is to investigate the mechanism of deflagration-to-detonation
transition in a detonation tube facility in the presence and absence of ignition promoters like ozone.
The factors governing such a transition will be studied for hydrogen-oxygen-diluent and ethyleneoxygen-diluent mixtures where the effect of congestion on this transition will be quantified. The effect
of ignition promoters on the ignition kinetics of a detonation wave structure will be investigated where
relevant length and time scales associated with a ZND detonation structure will be quantified for
hydrogen-oxygen-diluent and ethylene-oxygen-diluent mixtures.It is also proposed to carry out a series of thoughtful and well-planned experiments in a detonation tube to investigate the phenomenon of DDT. The primary goal here is to obtain a deeper understanding of the DDT phenomenon in scramjets and detonation-based rocket engines. Another aim of this work is to study the effect of ignition promoters like ozone on DDT lengths. The fuel sensitization experiments will be carried out in a detonation tube facility to investigate the effects of fuel sensitization on detonation wave structure and DDT lengths. |
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