Influence of ignition energy, ignition location, and stoichiometry on the deflagration-to-detonation distance in a Pulse Detonation Engine
The feasibility of utilizing detonations for air-breathing propulsion is the subject of a significant research effort headed by the Office of Naval Research. Pulse Detonation Engines (PDE) have a theoretically greater efficiency than current combustion cycles. However, pulse detonation technology mu...
Main Author: | Robinson, John P. |
---|---|
Other Authors: | Brophy, Christopher M. |
Language: | en_US |
Published: |
Monterey, California. Naval Postgraduate School
2012
|
Online Access: | http://handle.dtic.mil/100.2/ADA380632 http://hdl.handle.net/10945/9314 |
Similar Items
-
Experimental research into the influence of twospark ignition on the deflagration to detonation transition process in a detonation tube
by: Kostyantyn Korytchenko, et al.
Published: (2019-08-01) -
A Study of Deflagration To Detonation Transition In a Pulsed Detonation Engine
by: Chapin, David Michael
Published: (2006) -
Investigation of transient plasma ignition for a Pulse Detonation Engine
by: Rodriguez, Joel.
Published: (2012) -
Evaluation of straight and swept ramp obstacles on enhancing deflagration-to-detonation transition in pulse detonation engines
by: Medina, Carlos A.
Published: (2012) -
Ignition energy effect on detonation initiation by single and two successive ignitions
by: Wang Zhiwu, et al.
Published: (2020-01-01)