Lift Prediction of Spanwise Cambered Delta Wings
Author:
Affiliation:
1. Texas A&M University, College Station, Texas, 77843-3141
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2486
Reference17 articles.
1. 2Rom, J. “High Angle of Attack Aerodynamics,” Springer-Verlag, New York, 1991, pp.177-245.
2. Nonlinear Prediction of Aerodynamic Loads on Lifting Surfaces
3. Convergence characteristics of a vortex-lattice method for nonlinearconfiguration aerodynamics
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