Aerodynamic investigations of the freewing tilt-body UAV

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Galls, Samuel F ^a   Furey, Deborah A ^a   Rediniotis, Othon K ^a  

^a Department of Electrical and Computer Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTICAL MODELS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; ANTENNAS; AUTOMOBILE BODIES; UNMANNED AERIAL VEHICLES (UAV); WIND TUNNELS;

AERODYNAMIC PROPERTIES; CONTROL CHARACTERISTICS; FLIGHT CONDITIONS; HIGH ANGLE OF ATTACK; MOMENT MEASUREMENTS; REAL TIME MEASUREMENTS; WIND TUNNEL MODELING; WIND TUNNEL TESTS;

CONTROL SURFACES;

EID: 84983134012     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-759     Document Type: Conference Paper

References (6)

1. Barlow, J.B. & Chen, W., "Aerodynamic Characteristics and Control Aspects of a Freewing Tilt-Body Airplane," to be presented at the Twelfth Briston International Conference on RPVs, 9-11 September 1996, Bristol, UK.
2. Chen, W. & Barlow, J.B., "Stability, Control and Gust Response Characteristics of an Ultralight freewing Aircraft," AIAA-92-4342, Atmospheric Flight mechanics Meeting, Hilton Head, SC, August 10-12, 1992.
3. 1," AIAA-92-4194, AIAA Aircraft Design System Meeting, Hilton Head, SC, August 24-26, 1992.
4. Chen, W., "Stability, Control and Gust Sensitivity of a Low Wing Loading Freewing Airplane," M.S. Thesis, 1992.
5. Galls, S.F., Rediniotis, O.K. and Darmofal, D.L., "Development of An Interactive, Real-Time, Multimedia, Flow-Diagnostics Laboratory," AIAA Paper No. 96-0158, 34th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 1996.
6. Kinser, E. and Rediniotis, O.K., "Development of A Nearly-Omni-Directional, Three-Component Velocity Measurement Pressure Probe," AIAA Paper No. 96-0037, 34th AIAA Aerospace Sciences Meeting, Reno, Nevada, January 1996.