Thrust characteristics of an airbreathing pulse detonation engine in flight at mach numbers of 0.4 to 5.0 |
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| Authors: | A E Zangiev V S Ivanov S M Frolov |
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| Institution: | 1.Semenov Institute of Chemical Physics,Russian Academy of Sciences,Moscow,Russia;2.Center of Pulse Detonation Combustion,Moscow,Russia;3.National Nuclear Research University “MEPhI,”,Moscow,Russia |
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| Abstract: | Multidimensional calculations are performed to demonstrate that, by its characteristics, the pulse detonation engine (PDE) is a unique type of ramjet propulsion system, which can be used in both subsonic and supersonic aircraft. By a number of examples, it is shown that, in various thrust characteristics, such as the specific impulse, specific fuel consumption, and specific thrust, the PDE substantially exceeds ramjet engines. |
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