Aerothermal Shape Optimization of Hypersonic Vehicle Leading Edge by Using Genetic Algorithm
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aerothermal Analysis for Configuration Design of Swept Leading Edge Hypersonic Vehicle
Online Contents | 2016
|Aerothermal Analysis for Configuration Design of Swept Leading Edge Hypersonic Vehicle
Online Contents | 2016
|