Lift characteristics of the flapping wing micro air vehicle

Collection of Technical Papers - AIAA 3rd "Unmanned-Unlimited" Technical Conference, Workshop, and Exhibit

Volumn 1, Issue , 2004, Pages 127-135

  Muniappan, A ^a   Duriyanandhan, V ^a   Baskar, V ^a  

^a ANNA UNIVERSITY   (India)

Author keywords

[No Author keywords available]

Indexed keywords

DC MOTORS; LIFT; MANEUVERABILITY; REYNOLDS NUMBER; ROTORS; STRAIN GAGES; WINGS;

ACOUSTIC SENSORS; ANGULAR VELOCITY; FLAPPING FREQUENCY; MICRO AIR VEHICLES (MAV);

AEROSPACE VEHICLES;

EID: 19644385529     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Watkins, S., "Development of micro air vehicle," The Aeronautical Journal, Feb. 2003, pp. 117-123.
2. Woods, M. I., Hederson, J. F., and Lock, G. D., "Energy requirements of the flight of micro air vehicles," The Aeronautical Journal, Mar. 2001, pp. 135-149.
3. Tuncer, I. H., and Platzer, M. F., "Thrust Generation due to Airfoil Flapping," AIAA Journal, Vol.34, No. 2, Feb. 1996, pp. 324-331.
4. DeLaurier, J. D., and Harris, J.M., "Experimental Study of Oscillating-Wing Propulsion," J. AIRCRAFT, Vol. 19, No.5, May 1982, pp. 368-373.
5. Rae, W.H., and Pope, A., Low Speed wind Tunnel Testing, John Wiley Publication, 1984
6. Dally, J.W., and Riley, W.F., Experimental Stress Analysis, McGraw Hill Inc., New York, 1978
7. Baskar, V., and Muniappan, A., "Development of flapping mechanism for micro air vehicle," International Conference on Mechanical Engg. (ICME-2003), ICME-2003 FL-10, BUET, Bangladesh, Dhaka, Dec. 26-28, 2003.
8. nd Aerospace Sciences and Exhibit, AIAA, 2004-40, Reno, Nevada, Jan. 5-8, 2004.