Aerodynamic characteristics of unmanned aerial vehicles and its shape design

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 27, Issue 2, 2006, Pages 161-174

  Zhu, Zi Qiang ^a   Wang, Xiao Lu ^a   Chen, Ze Min ^a   Wu, Zong Cheng ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aerodynamic design; Aerodynamics; Unmanned aerial vehicle

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; DESIGN; LAMINAR FLOW; OPTIMIZATION; PROPULSION; THREE DIMENSIONAL; UNMANNED VEHICLES; WINGS;

AERODYNAMIC DESIGN; HYBRID DESIGN IDEA; MULTIOBJECTIVE MULTIPOINT OPTIMIZATION DESIGN METHOD; UNMANNED AERIAL VEHICLES (UAV);

AIRCRAFT;

EID: 33745121568     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

1. Zhu Z Q, Wu Z C. Aerodynamics for modern aircraft design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2005. (in Chinese)
2. Batkov A M. Experiences of using UAV in local military conflict and its effect in the 21th aeronautic area[A], The Second Sino-Russia Academic Proseminar on UAV[C]. 2005.
3. Zhu Z Q, Wang X L, Wu Z C, et al. Aerodynamic characteristics of small and micro unmanned aerial vehicles and its shape design[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(3) (to be published), (in Chinese)
4. Stein M, Shepshelovich M. Development of UAV wings-transonic design[R]. AIAA 2005-42, 2005.
5. Liu Z, Zhu Z Q, Fu H Y, et al. Design of airfoil with high ratio of lift over drag[J]. Acta Aerodynamica Sinica, 2004, 22(4): 410-415. (in Chinese)
6. Wang X L, Zhu Z Q, Liu Z, et al. Bi-point (BP)/bi-objective (BO) optimization design of ailfoil using N-S equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006. (to be published), (in Chinese)
7. Li P, Om D. Design application in the industry[A]. IUTAM Symposium Transsonicum IV[C]. Kluwer Academic Publishers, 2003. 231-238.
8. Shelton A, Tomar A, Prasad J V R, et al. Active multiple winglets for improved UAV performance[R]. AIAA 2004-4968, 2004.
9. Cummings R M, Morton S A, Siegel S G, et al. Numerical prediction and wind tunnel experiment for a pitching unmanned combat air vehicle[R]. AIAA 2003-0417, 2003.
10. Zhan G. Overall project analysis of X-45C and X-47B American UCAV[A]. The Second Sino-Russia Academic Proseminar on UAV[C]. 2005. (in Chinese)
11. Zhu Z Q, Li H M, Li J, et al. Discussions on bidisciplinary (aerodynamics/electromagnetics) optimization methods[J], Acta Mechanica, 2000, 143: 17-33.
12. Xia L. Research on aircraft shape aerodynamic/stealthy integral optimization design method[D]. Xi'an: Northwestern Polytechnical University, 2004. (in Chinese)
13. Chen Z M, Zhu Z Q, Wu Z C. N-S solution of flow around three-dimensional spoilers[J], (to be published), (in Chinese)