DOI QR코드

DOI QR Code

CFD 해석 및 최적화 기법을 이용한 피토관 형상설계

Design of Pitot-Tube Configuration Using CFD Analysis and Optimization Techniques

  • 김도준 (경상대학교 대학원 기계항공공학부) ;
  • 천영성 (경상대학교 대학원 기계항공공학부) ;
  • 명노신 (경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 박찬우 (경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 조태환 (경상대학교 및 항공기부품기술연구소) ;
  • 박영민 (한국항공우주연구원) ;
  • 최인호 (한국항공우주연구원)
  • 발행 : 2008.05.01

초록

Accurate measurement of speed and altitude of flying vehicles in air data system remains a critical technical issue. A highly reliable Pitot-static probe is required to obtain air data such as total pressure and static pressure. In this study, an analysis of the characteristics of flowfield around the Pitot-static probe was performed by using a Navier-Stokes CFD code. In addition, for the purpose of finding an optimal configuration, a technique based on the response surface method is applied to the problem with design parameters including shape of the nose section and cone angle. It is shown that the optimal configuration fulfills the MIL specification in wider range of high angles of attack.

키워드

참고문헌

  1. Gracey, W., 1981, "Measurement of Aircraft Speed and Altitude," John Wiley & Sons
  2. Boetcher, S. K. S. and Sparrow, E. M., 2007, "Limitations of the Standard Bernoulli Equation Method for Evaluating Pitot/Impact Tube Data," Int. J. of Heat and Mass Transfer, Vol. 50, pp. 782-788 https://doi.org/10.1016/j.ijheatmasstransfer.2006.01.044
  3. "FLUENT User's Guide," FLUENT Inc, 1998
  4. Baldwin, B. S. and Barth, T. J., "A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows," AIAA Paper 91-0610
  5. Klaus, A. Hoffmann, 2000, "Computational Fluid Dynamics Volume III," 4th Edition, EESbooks
  6. Gracey, W., Letko, W. and Russel, W. R., 1951, "Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angle of Attack . Subsonic Speed," NACA TN 2261
  7. Myers, R. H., 1995, "Response Surface Methodology," John Wiley & Sons Inc
  8. "Design Expert 6.0 User's Guide," Response Surface Method (RSM) Tutorials, 2003
  9. Gracey, W., Elwood, S., 1951, "Flight Inves tigation of the Variation of Static-Pressure Error of a Static-Pressure Tube with Distance Ahead of a Wing and a Fuselage," NACA TN 2311
  10. Lee, S. W. and Yoon, T. J. 1997, "Experimental Investigation of Flow Parameters Influencing the Calibration of Five-Hole Prebes," J. of KSME(B), Vol. 21, No. 5, pp. 637-649
  11. Lee, S. W. and Yoon, T. J. 1996, "Effect of Wall Proximity on the Calibration of a Miniature Cone-Type Five-Hole Probe," J. of KSME(B), Vol. 20, No. 8, pp. 2693-2706
  12. "Pitot-Static Tube, L-Shaped, Compensated General Specification for Military Specification," MIL-P-83206B, 31 1978