The Principal Aspects of Application of Detonation in Propulsion Systems
Author(s) -
А. А. Васильев
Publication year - 2013
Publication title -
journal of combustion
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.45
H-Index - 18
eISSN - 2090-1968
pISSN - 2090-1976
DOI - 10.1155/2013/945161
Subject(s) - detonation , deflagration to detonation transition , deflagration , impulse (physics) , propulsion , mechanics , specific impulse , supersonic speed , aerospace engineering , nuclear engineering , physics , engineering , classical mechanics , chemistry , explosive material , organic chemistry
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
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom