Lateral aerodynamics of delta wings with leading-edge separation
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference23 articles.
1. Vortex-Lattice Method for the Calculation of the Nonsteady Separated Flow over Delta Wings
2. Method for calculating wing loading during maneuvering flight along a three-dimensional curved path
3. A discrete vortex method for the non-steady separated flow over an airfoil
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