@inbook{59614bed000441eea400c8ca2f6e29a5,
title = "Propulsion: Design and Testing of Gasdynamically Optimized Fuel Injectors for the Piloting of Supersonic Flames with Low Losses",
keywords = "Airbreathing propulsion systems, Dual-mode combustion, Gasdynamically optimized fuel injectors, Hypersonic inlets, Hypersonic propulsion systems, Lobed strut injectors, Nozzle flow fields, PDF/FDF-methods, Propulsion, Research, Supersonic and hypersonic transport, Supersonic combustion, Supersonic flames, Supersonic turbulent combustion, Systems off-design simulation, Technologies for two-stage-to-orbit vehicles, Viscous interaction effects",
author = "Anatoliy Lyubar and Tobias Sander and Thomas Sattelmayer",
year = "2005",
month = nov,
day = "7",
doi = "10.1002/3527605711.ch5",
language = "English",
isbn = "3527277358",
pages = "284--307",
booktitle = "Basic Research and Technologies for Two-Stage-to-Orbit Vehicles",
publisher = "John Wiley and Sons",
}