Numerical Simulations of an Airplane with an Active Flow Control System
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3929
Reference13 articles.
1. 1Rathay, N. W., Boucher, M. J, Amitay, M. and Whalen, E. "Performance Enhancement of a Vertical Tail Using Synthetic Jet Actuators," AIAA Paper 2012-71.
2. 2Rathay, N.W., Boucher, M. J., Amitay, M. and Whalen, E. "Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-zero Sideslip," AIAA Paper 2012-2657.
3. 3Seele, R., Graff, E., Gharib, M., Taubert, L., Lin, J. and Wygnanski, I.L. "Improving Rudder Effectiveness with Sweeping Jet Actuators", AIAA Paper 2012-3244.
4. 4Seele, R., Graff, E., Lin, J. and Wygnanski, I.L. "Performance Enhancement of a Vertical Tail Model with Sweeping Jet Actuators", AIAA Paper 2013-0411.
5. 5Whalen, E., Shmilovich, A., Spoor, M., Tran, J., Vijgen, P., Lin, C.J. and Andino, M. "Full-scale Flight Demonstration of an Active Flow Control Enhanced Vertical Tail," AIAA Paper 2016-3927.
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1. Numerical Study on Lift Enhancement for Upper Surface Blowing System with Powered Turbofan Engine;AIAA Aviation 2019 Forum;2019-06-15
2. Practical Computational Methods for Airplanes with Flow-Control Systems;AIAA Journal;2019-01
3. Technique for Enhanced Flow Control Efficiency Through Thermal Actuation;AIAA Journal;2018-09
4. Flight Test of an Active Flow Control Enhanced Vertical Tail;AIAA Journal;2018-09
5. Schlieren Visualization and Analysis of Sweeping Jet Actuator Dynamics;AIAA Journal;2018-08
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