The Optimization Design of a Compact Integrated Precooler for Advanced Space Launcher Engines
In recent years, aeroplane engines have evolved towards the direction of hypersonic flight, re-use and combined cycle propulsion. As one of the core components, air-hydrogen precooler plays a vital role in the development of liquefied air cycle engines. In order to solve the problem of rapid cooling...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
AIDIC Servizi S.r.l.
2020-08-01
|
| Series: | Chemical Engineering Transactions |
| Online Access: | https://www.cetjournal.it/index.php/cet/article/view/11006 |