Effects of wing planforms on aerodynamics of MAV

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

Volumn 25, Issue 4, 2007, Pages

  Wang, Jin Jun ^a   Tu, Jian Qiang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aerodynamic performance; Low aspect ratio wing; MAV; Planform

Indexed keywords

ASPECT RATIO; DRAG; LIFT; WIND TUNNELS; WINGS;

MICRO AIR VEHICLES (MAV); SPANWISE LENGTH; STALLING ANGLE; SWEEP ANGLES;

AERODYNAMICS;

EID: 40049099572     PISSN: 02581825     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

1. TAYLOR G S, SCHNORBUS T, GURSUL I. An investigation of vortex flows over low sweep delta wings [R]. AIAA-2003-4021, June 2003.
2. TAYLOR C S, KORKER A, CURSUL I. Passive flow control over flexible non-slender della wings [R]. AIAA-2005-0865, 2005.
3. GORDNIER R E, AND VISBAL M R. Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow [R]. AIAA 2003-0620, 2003.
4. PELLETIER A, AND MUELLER T J. Low Reynolds number aerodynamics of LAR, thin/flat/cambered-plate wings [J]. Journal of Aircraft, 2000, 37(5): 825-832.
5. TORRES G E, AND MUELLER T J. LAR wing aerodynamics at low Reynolds numbers [J]. AIAA Journal, 2004, 42(5): 865-873.
6. BOLLAY W. A non-linear wing theory and its application to rectangular wings of small aspect ratio [J]. Zeitschrift Fur Angewandte Malhematikund Mechanik, 1939, 19: 21-35.
7. POLHAMUS E C. A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogy [R]. NASA TN D-3767, 1966.
8. POLHAMUS E C. Predictions of vortex-lift characteristics by a leading-edge-suction analogy [J]. Journal of Aircraft, 1971, 8(4): 193-199.
9. LAMAR J E. Predictions of vortex flow characteristics of wings at subsonic and supersonic speeds [J]. Journal of Aircraft, 1976, 13(7): 490-494.
10. LAMAR J E. Extension of leading-edge-suction analogy to wings with separated flow around the side edge at subsonic speeds [R]. NASA TR R-428, 1974.
11. WANG J J, ZHAN J X. New pair of leading edge vortex for flow over delta wing [J]. Journal of Aircraft, 2005, 42(3): 718-721.
12. WANG J J, LU S F. Effects of leading-edge bevel on the aero-dynamic forces of non-slender delta wing [J]. The Aeronautical Journal, 2005, 109(8): 403-407.