@inproceedings{0814b4dd4d524f8b880e246fa8faeab9,
title = "A Wide-range single engine: Operated from startup to hypersonic",
abstract = "A single lightweight engine capable of operating over a wide range of Mach numbers from startup to the hypersonic regime is proposed for aircrafts and spaceships. A compression system of colliding super multijets is proposed instead of a traditional turbofan. Computational fluid dynamics with a chemical reaction model clarifies a large potential and stability of this system. This ultimate engine system can be extended with a special piston and scram jet systems to achieve an improved fuel consumption rate at various situations between the ground and the space, while maintaining a very low noise level with silent detonation. The present engine system will also solve the problem of the buzz at highersonic conditions.",
author = "Ken Naitoh and Kazushi Nakamura and Takehiro Emoto",
year = "2011",
doi = "10.2514/6.2011-2316",
language = "English",
isbn = "9781600869426",
series = "17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011",
booktitle = "17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011",
note = "17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011 ; Conference date: 11-04-2011 Through 14-04-2011",
}