DOI QR코드

DOI QR Code

A Study on Transient Characteristics of Flow Caused by Heat Addition in Supersonic Nozzle

초음속 노즐 내부 유동장의 가열에 의한 천이 특성에 대한 연구

  • 정진도 (호서대학교 환경안전공학부) ;
  • 김장우 (호서대학교 환경안전공학부)
  • Published : 2005.01.01

Abstract

This study presents numerical solutions of the two-dimensional Navier-Stokes equations for supersonic unsteady flow in a convergent-divergent nozzle with heat addition. The TVD scheme in generalized coordinates is employed in order to calculate the moving shock waves caused by thermal choking. We discuss on transient characteristics, start and unstart phenomena, fluctuations of specific thrust caused by thermal choking and viscous effects. We prove that the control of separation of boundary layer is the most important key problem to prevent the thermal choking.

Keywords

References

  1. White, M. E., Drummond J. P. and Kumar A., 1987, 'Evolution and Application of CFD Techniques for Scramjet Engine Analysis,' Journal of Propulsion and Power, Vol. 3, No.5, pp. 423-439 https://doi.org/10.2514/3.23007
  2. Heiser, W. H. and Pratt, D. T., 1994, Hypersonic Airbreathing Propulsion, AIAA Education Series, Washington, D. C., pp. 76-86
  3. Heiser, W. H., McClure, W. B. and Wood, C. W., 1994, 'Simulating Heat Addition via Mass Addition in Constant Area Compressible Flows,' AIAA Journal, Vol. 33, No.1, pp. 167-171 https://doi.org/10.2514/3.12352
  4. Onodera, T. and Kaji, S., 1994, '2-Dimensiona1 Numerical Analysis of the Interacting Between Scramjet Engine Modules,' Journal of The Japan Society for Aeronautical and Space Science, Vol. 42, No. 480, pp. 53-59 https://doi.org/10.2322/jjsass1969.42.53
  5. Yoon, Y., Donbar, J. M., Huh, H. and Driscoll, J. F., 1996, 'Measured Supersonic Flame Properties: Heat-Release Patterns, Pressure losses, Thermal Choking Limits,' Journal of Propulsion and Power, Vol. 12, No.4, pp. 718-723 https://doi.org/10.2514/3.24093
  6. Kim, J. W. and Chung, J. D., 2002, 'A Numerical Study on Characteristics of Unsteady Flows Caused by Heat Addition in a Convergent-Divergent Duct,' Trans. of the KSME (B), Vol. 26, No.6, pp. 765-771 https://doi.org/10.3795/KSME-B.2002.26.6.765
  7. Stull, D. R. and Prophet, H., 1964, JANAF Thermochemical Tables, U. S. Department of Commerce, Washington, D. C.
  8. Roe, P. L. (1981). 'Approximate Riemann Solvers, parameter vectors, and difference schemes,' Journal of Computational Physics, Vol. 43, pp.357-372 https://doi.org/10.1016/0021-9991(81)90128-5
  9. Yee, H. C. and Harten, A., 1987, 'Implicit TVD Schemes for Hyperbolic Conservation Laws in Curvilinear Coordinate,' AIAA Journal, Vol. 25, No.2, pp. 266-274 https://doi.org/10.2514/3.9617
  10. Anderson, D. A., Tannehill, J. C. and Pletcher, R. H., 1984, Computational Fluid Mechanics and Heat Transfer, Hemisphere Publishing Corporation, New York, pp. 479-489
  11. Johnson, D. A. and King, L. S., 1985, 'A Mathematically Simple Turbulence Closure Model for Attached and Separated Turbulent Boundary Layers,' AIAA Journal, Vol. 23, No. 11, pp. 1684-1692
  12. Abid, R., Vatsa, V. N., Johnson, D. A. and Wedan, B. W., 1990, 'Prediction of Separated Transonic Wing Flows with Non-Equilibrium Turbulence Model,' AIAA Journal, Vol. 28, No.8, pp. 1426-1431 https://doi.org/10.2514/3.25234
  13. Noguchi, Y. and Shiratori, T., 1994, 'Behavior of the Johnson-King Turbulence Model in Axisymmetric Supersonic Flows,' AIAA Journal, Vol. 32, No.7, pp. 1394-1398 https://doi.org/10.2514/3.12207