Zonal Detached Eddy Simulation of a Civil Aircraft with a Deflected Spoiler
Author:
Affiliation:
1. Applied Aerodynamics Department, ONERA—The French Aerospace Lab, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052106
Reference19 articles.
1. Numerical Spoiler Wake Investigations at the Borders of the Flight Envelope
2. also AIAA Paper 1982-127.
3. also AIAA Paper 1981-72.
4. also AIAA Paper 1983-2131.
5. Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence Models
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