Lateral aerodynamics of delta wings with leading edge separation

Author:

KATZ J.1

Affiliation:

1. Technion - Israel Institute of Technology, Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Tobak, M. and Schiff, L.B."A Nonlinear Aerodynamic Moment Formulation and i t s Implications for Dynamic Stability Testing". AIAA paper No. 71-275.

2. Tobak, M. and Schiff, L.B. "Nonlinear Aerodynamics of Aircraft in High-Angle-of-Attack Maneuvers. AIAA paper No. 74-85.

3. Levin, D. and Katz, J. "A Vortex-Lattice Method for the Cilculation of the Elonsteady Separated Flow over Delta Wings". AIAA paper 80-1803.

4. Method for calculating wing loading during maneuvering flight along a three-dimensional curved path

5. A discrete vortex method for the non-steady separated flow over an airfoil

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