Experimental aerodynamics of mesoscale trailing-edge actuators

AIAA Journal

Volumn 40, Issue 12, 2002, Pages 2538-2540

  Solovitz, Stephen A ^a   Eaton, John K ^a  

^a Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; BOUNDARY LAYERS; CONTROL SYSTEMS; REYNOLDS NUMBER; TURBULENCE; WIND TUNNELS;

FLAP; FLEXIBLE WING; MESOSCALE TRAILING EDGE ACTUATORS; MINIATURE TRAILING EDGE EFFECTORS;

WINGS;

EID: 0036935190     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1600     Document Type: Article

References (7)

1. Kroo, I. M., "Aerodynamic Concepts for Future Aircraft," AIAA Paper 99-3524, June 1999.
2. Storms, B. L., and Jang, C. S., "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators," Journal of Aircraft, Vol. 31, No. 3, 1994, pp. 542-547.
3. Liebeck, R. H., "Design of Subsonic Airfoils for High Lift," Journal of Aircraft, Vol. 15, No. 9, 1978, pp. 547-561.
4. Myose, R., Papadakis, M., and Heron, I., "Gurney Flap Experiments on Airfoils, Wings, and Reflection Plane Model," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 206-211.
5. Yen-Nakafuji, D. T., van Dam, C., Michel, J., and Morrison, P., "Load Control for Turbine Blades: A Non-Traditional Microtab Approach," AIAA Paper 2002-0054, Jan. 2002.
6. Park, B., "Miniaturization of Functional Mechanisms with SDM Processing," Ph.D. Dissertation, Dept. of Mechanical Engineering, Stanford Univ., Stanford, CA, Jan. 2002.
7. Solovitz, S. A., "Experimental Aerodynamics of Mesoscale Trailing-Edge Actuators," Ph.D. Dissertation, Dept. of Mechanical Engineering, Stanford Univ., Stanford, CA, Dec. 2002.