A range of aerodynamic analyses are introduced to enable the initial spreadsheet calculations to be refined. These are chiefly based on the panel codes XFoil and XFLR5 and the RANS CFD code Fluent. Depending on the sophistication and budget of the design team, this process can be quite lightweight or can involve significant computational runs.
Preliminary Aerodynamic and Stability Analysis
2017-10-23
41 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Aerodynamic preliminary analysis
NTRS | 1981
|Preliminary measurements of aircraft aerodynamic noise
NTRS | 1974
|Aerodynamic Modeling for Global Stability Analysis
AIAA | 2002
|