Design and flight test of a fixed wing MAV

1st UAV Conference

Volumn , Issue , 2002, Pages

  Hwang, H C ^a   Chung, D K ^a   Yoon, K J ^a   Park, H C ^a   Lee, Y J ^a   Kang, T S ^a  

^a Konkuk University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINE SYSTEMS; FLIGHT TEST; LOWER NOISE; WING SPAN;

ELECTRIC MOTORS; MICRO AIR VEHICLE (MAV); PARTIAL DISCHARGES;

FIXED WINGS;

EID: 84896899032     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Joel M. Grasmeyer, Matthew T. Keenoon, Development of the Black Widow Micro Air Vehicle, AIAA-2001-0127, 2001
2. Mark Dre la (MIT Aero & Astro), XFOIL v6.91, Oct. 2000
3. Daniel P. Raymer, "Aircraft Design: A Conceptual Approach", 3rd edition, 1999
4. J. Seddon, "Basic Helicopter Aerodynnmics", 1990, Marston Book Services, Ltd.
5. Wilbur C. Nelson "Airplane Propeller Principles", 1943
6. Peter G. Ifju, Scott Ettinger, David Jenkins, Luis Martinez, "Composite Materials for Micro Air Vehicles", SAMPE Journal, Vol. 37, No. 4, July/August 2001