Multipoint Optimisation of Coanda Surfaces for Transonic Circulation Control using the Adjoint Method

Author:

Forster Matthew1,Biava Massimo2,Steijl Rene2

Affiliation:

1. University of Liverpool

2. University of Glasgow

Publisher

American Institute of Aeronautics and Astronautics

Reference37 articles.

1. Development of advanced circulation control wing high-lift airfoils

2. A circulation control actuator for flapless flight control

3. High-speed characteristics of circulation control airfoils

4. 4Alexander, M. G., Anders, S. G., Johnson, S. K., Florance, J. P., and Keller, D. F. "Trailing Edge Blowing on a Two-Dimensional Six-Percent Thick Elliptical Circulation Control Airfoil up to Transonic Conditions," Tech. Rep. TM-2005-213545, NASA, 2005.

5. 5Wenzinger, C. J. and Harris, T. A. "Wind-Tunnel Investigation of an NACA 23012 Airfoil with Various Arrangements of Slotted Flaps," Tech. Rep. NACA-TR-664, NACA, 1939.

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