Transonic Nacelle Aerodynamic Optimization Based on Hybrid Genetic Algorithm (AIAA 2016-3833)
17th AIAA-ISSMO Multidisciplinary Analysis and Optimization Conference 2016 ; 2016 ; Washington, D.C.
01.01.2016
9 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection (AIAA 2015-3833)
British Library Conference Proceedings | 2015
|Frequency Domain Approach for Transonic Aerodynamic Modelling (AIAA 2016-1576)
British Library Conference Proceedings | 2016
|DataCite | 1919
British Library Conference Proceedings | 2016
|