Computational Method in the Throughflow Simulation of Aeroengine Compressor
Aerospace system science and engineering (4th international conference)
2021-01-01
14 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Computational Method in the Throughflow Simulation of Aeroengine Compressor
Springer Verlag | 2021
|A Database of Optimal Airfoils for Axial Compressor Throughflow Design
Online Contents | 2017
|A ROBUST DESIGN METHODOLOGY FOR HIGH-PRESSURE COMPRESSOR THROUGHFLOW OPTIMIZATION
British Library Conference Proceedings | 2003
|Viscous Throughflow Modeling for Multistage Compressor Design (92-GT-302)
Online Contents | 1993
|