Unsteady High-Angle-of-Attack Aerodynamic Models of a Generic Jet Transport
Author:
Affiliation:
1. Department of Mechanical Engineering, The Cooper Union, New York, New York 10003
2. Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey 08544
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032976
Reference12 articles.
1. VassbergJ. C.DeHaanM. A.RiversS. M.WahlsR. A. “Development of a Common Research Model,” AIAA Paper 2008-6919, 2008.
2. State-space representation of aerodynamic characteristics of an aircraft at high angles of attack
3. A Unified Baseline Grid about the Common Research Model Wing/Body for the Fifth AIAA CFD Drag Prediction Workshop (Invited)
4. Two-equation eddy-viscosity turbulence models for engineering applications
5. Computational Aerodynamics: Solvers and Shape Optimization
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