z-logo
open-access-imgOpen Access
Tailored Fuel Injection for Pulsed Detonation Engines via Feedback Control
Author(s) -
Alberto Aliseda,
Kartik B. Ariyur,
Olivier Sarrazin,
Juan C. Lasheras,
Miroslav Krstić
Publication year - 2003
Publication title -
journal of propulsion and power
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.913
H-Index - 101
eISSN - 1533-3876
pISSN - 0748-4658
DOI - 10.2514/2.6184
Subject(s) - detonation , materials science , fuel injection , automotive engineering , engine knocking , nuclear engineering , aerospace engineering , ramjet , combustion , combustion chamber , engineering , explosive material , combustor , homogeneous charge compression ignition , chemistry , organic chemistry
An architecture is developed for feedback regulation of liquid volume fraction proe les in an air jet cone ned in a tube. The application to the controlled injection of fuel in detonation tubes for pulsed detonation engines is considered.Thearchitectureconsistsoflaserattenuationsensing ofliquidvolumefractionalongthetube,actuation on the liquid injection pressure through an array of solenoidal valves, and proportional‐ integral feedback. The architecture is validated by means of cold-e ow experiments regulating the concentration proe le of water droplets along the detonation tube to desired values.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom