Analysis on Aerodynamic Characteristics of the CRW Air-Vehicle

CRW 비행체의 공력특성 해석

  • Published : 2003.12.01

Abstract

Smart UAV Development Program, one of the 21c Frontier R&D Program sponsored by MOST(Ministry of Science and Technology), was launched in 2002 As an air vehicle for the Smart UAV, CRW(Canard Rotor/wing) concept was one of the candidates compared in trade-off study. The CRW concept has not only been proven completely but its aerodynamic characteristics not known in detail yet. Two calculation methods were adopted in this study to obtain aerodynamic data for the CRW First method was the superpose DATCOM method which is capable of three lifting sufaces, and second one is the full Navier-Stokes computation around CRW configuration using overset grid method. Basic aerodynamic characteristics of the CRW configuration was analyzed and the minimum drag level with lift to drag ratio is presented. The peculiar flow characteristics around rotor/wing and hub were also examined and considered in the configuration design.

Keywords

References

  1. Bass, S. M., Thompson, T. L., Rutherford, J. W., and Swanson, S., 'Low-Speed Wind Tunnel Test Results of the Canard Rotor/Wing Concept,' AIAA-93-3412
  2. Thompson, T. L., Smith, R. L., Helwani, M., and Shockey, G. A., 'Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration,' 57th AHS Forum, WA, May 9-11, 2001
  3. 장병희, 조상오, 박영민, 'DATCOM과 중첩 기법을 이용한 스마트무인기 El 형상에 대한 공력계산,' SUDC-ED-B21-01-003-R0, 2003.3
  4. Pandya, S. A. and Aftomis, M. J., 'Computation of Extemal Aerodynamics for a Canard Rotor/Wing Aircraft,' AIAA 2001-0997
  5. Pulliam, T. H. and Chaussee, D. S., 'A Diagonal Form of an Implicit ApproXimate-Factorization Algorithm', Joumal of Computational Physics, Vo1.39, Feb., 1981, pp. 347-363
  6. Boeing Phantom Works X-50A Document, 2002
  7. Jane's Unmanned Aerial Vehicles and Targets, Issue Sixteen, 2001
  8. 황수정, 안오성, 'Configuration El,' SUDC-ED-B1-01-001-R1, 2002. 12