Unmanned Aerial Vehicle (UAV) with plasma actuators for separation control

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Grundmann, Sven ^a   Frey, Michael ^a   Tropea, Cameron ^a  

^a DARMSTADT UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT CONTROL; ANTENNAS; FLOW SEPARATION; LAMINAR BOUNDARY LAYER; TURBOMACHINE BLADES; UNMANNED AERIAL VEHICLES (UAV);

ACTIVE CANCELLATIONS; CONTROL APPLICATIONS; FLIGHT EXPERIMENTS; HEAVY EQUIPMENT; HIGH VOLTAGE GENERATORS; LAMINAR TO TURBULENT TRANSITIONS; SEPARATION CONTROL; TOLLMIEN-SCHLICHTING WAVES;

WINGS;

EID: 78349300427     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-698     Document Type: Conference Paper

References (4)

1. Roth, J., Sherman, D., and Wilkinson, S., "Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma," 36th Aerospace Sciences Meeting & Exhibit, 12-15 January, Reno, Nevada, No. AIAA 98-0328, 1998.
2. Roth, J., "Electrohydrodynamically induced airflow in a one atmosphere uniform glow discharge surface plasma," 25th IEEE Int. Conf. Plasma Science (Raleigh, USA), 1998.
3. Moreau, E., "Airflow control by non-thermal plasma actuators," Journal of Physics D: Applied Physics, Vol. 40, No. 3, 2007, pp. 605-636.
4. Frey, M., "Auslegung, Konstruktion, Bau und Erprobung eines unbemannten Kleinflugzeuges (MAV) mit Plasma Aktuatoren zur Zirkulationskontrolle am Tragflügel," Bachelor's Thesis, Technische Universität Darmstadt, 2008.