Comparison of Numerical Results With Wind Tunnel Aerodynamic Data of Flight Vehicle for Hypersonic Flight
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Free-flight wind tunnel for aerodynamic testing at hypersonic speeds
Engineering Index Backfile | 1955
|Aerodynamic Characteristics Evaluation of Hypersonic Flight Experiment Vehicle Based on Flight Data
Online Contents | 1997
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