International Journal of Aeronautical and Space Sciences

  • 제7권1호
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  • Pages.27-42
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  • 2006
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Supersonic Plug Nozzle Design and Comparison to the Minimum Length Nozzle Configuration

  • 발행 : 2006.06.30
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초록

A method to design the contour and conception of a plug nozzle of arbitrary shape, but specified exit flow conditions is presented. Severals shapes can be obtained for exit Mach number by changing the specific heats ratio. The characteristics of the nozzle in terms of length, weight and pressure force exerted on the wall are compared to the Minimum Length Nozzle and found to be better. Our field of study is limited to the supersonic mode to not to have the dissociation of the molecules. The design method is based on the use of the Prandtl Meyer function of a perfect gas. The flow is not axial at the throat, which may be advantageous for many propulsion applications. The performance benefits of the plug nozzle compared to the Minimum Length Nozzle are also presented.

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참고문헌

  1. Shapiro A. H., 'Compressible Fluid Flow, 'Vol. 1. New York, the Ronald Press, 1953
  2. Hill P. G. and Peterson C.R.. 'Mechanical and Thermodynamics of Propulsion', Addition-Wesley Publishing Company Inc.. New York, 1965
  3. J. D. Anderson Jr.. 'Modern Compressible flow. With Historical Pers pective', 2nd ed., Mc Graw-Hill Book Company, New York, 1982
  4. J. D. Anderson Jr., 'Fundamentals of Aerodynamics', 2nd ed.. Mc Graw-: Hill Book Company, New York, 1988
  5. Rao G.V.R.. 'Recent Developments in Rocket Nozzle Configuration', ARS Journal. Nov.. 1961. pp. 1488. 1491
  6. Michael F. and Robert H.. 'Performance aspects of plug cluster nozzles', Journal of Spacecraft And Rockets. Vol. 33, No. 4, 1996, pp. 507, 512 https://doi.org/10.2514/3.26792
  7. Rommel T., Hagemann G., Schley C. A., Kruelle G., and Manski D., 'Plug Nozzle Flowfield Analysis', Journal of Propulsion and Power, Vol. 13, No. 5, 1997, pp. 629, 634 https://doi.org/10.2514/2.5227
  8. Francesco N. and Marcello. O.. 'Methodology to Solve Flowfields of Plug Nozzles for Future Launchers', Journal of Propulsion and Power, Vol. 14, No. 3, 1998, pp. 318, 326 https://doi.org/10.2514/2.5300
  9. Gerald H.. Hans I.. Thong V.N.. and Gennady E. D., 'Advanced Rocket Nozzles', Journal of Propulsion and Power, Vol. 11, No. 5, 1998, pp. 620, 634
  10. Francesco N. and Marcello O.. 'Theoretical Analysis and Engineering Modeling of Flowfields in Clustered Module Plug Nozzles', Journal of Propulsion and Power, Vol. 15, No. 4, 1999, pp. 544, 551 https://doi.org/10.2514/2.5477
  11. Korte J. J.. Salas A. O., Dunn H. J., Alexandrov N. M., Follett W. W., Orient G. E. and Hadid A. H., 'Multidisciplinary Approach to Linear Aerospike Nozzle Design', Journal of Propulsion and Power, Vol. 17, No. 1. 2001. pp. 93, 98 https://doi.org/10.2514/2.5712
  12. Kraiko A. N., Tillyayeva N. I. and Baftalovskii S.. V, 'Optimal Design of Plug Nozzles and Their Thrust Determination at Start', Journal of Propulsion and Power, Vol. 17, No. 6, 2001. pp. 1347. 1352 https://doi.org/10.2514/2.5885
  13. Takashi I., Fujii K., Hayashi A. K., 'Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structures and Thrust Performance', Journal of Propulsion and Power, Vol. 18, No. 2, 2002, p. 254-260 https://doi.org/10.2514/2.5964
  14. Menko E. N. W. and Willem J. B., 'Trailing-Edge Cavity Afterbodies for Linear Plug Nozzle Engines', AIAA Journal, Vol. 41, No. 9, 2003, pp. 1715, 1721 https://doi.org/10.2514/2.7317
  15. Hagemann G., Immich H. and Terhardt M., 'Flow phenomena in advanced rocket nozzles - The plug nozzle', AIAA-1998-3522, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, OH, July 13-15, 1998
  16. Marsilio R., 'Numerical simulations for plug nozzle flowfield', AIAA-2001-670, 39th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 8-11, 2001
  17. Zebbiche Too 'Supersonic Plug Nozzle Design,' AIAA-2005-4490, 41th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Arizona, July 10-13, 2005
  18. Onofri M., 'CFD Results of Plug Nozzle Test Cases', AIAA-2002-4036, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana, July 7-10, 2002
  19. Wisse M., van Oudheusden B. and Bannink W., 'Analytical Optimisation of an Inviscid Flow Linear Plug Nozzle Boattail', AIAA-2004-4017, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, July 11-14, 2004
  20. Greer, H., 'Rapid Method for Plug Nozzle Design', ARS Journal. April 1961, pp. 560-561
  21. Angelino, G., 'Approximate Method for Plug Nozzle Design', AIAA Journal, Vol. 2, N${\circ}$ 10, 1964, pp. 1834-1835 https://doi.org/10.2514/3.2682
  22. Rao, G. V. R., 'Spike Nozzle Contour for Optimum Thrust', Ballistic Missile and Space Technology, edited by C. W. Morrow, Vol. 2. Pergamon Press, New York, 1961, pp. 92-101