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Development and Calibration of Detonation-Driven High-Enthalpy and Hypersonic Test Facilities

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Abstract

Hypersonics for the foreseeable future is the domain of space access and hypersonic flight. A hypersonic vehicle encounters an aero-thermodynamic environment characterized by strong shocks and high temperatures, and the flow in the hypersonic regime behaves quite differently from that at supersonic Mach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, 1994; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, 1989; Anderson in Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York, 1989).

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References

  1. Bertin, J.J.: Hypersonic Aerothermodynamics. AIAA Education Series, Washington DC (1994)

    Google Scholar 

  2. Park, C.: Nonequilibrium Hypersonic Aerothermodynamics. Wiley, New York (1990)

    Google Scholar 

  3. Anderson, J.D.: Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York (1989)

    Google Scholar 

  4. Bertin, J.J., Cummings, R.M.: Fifty years of hypersonics: Where we’ve been, where we’re going. Prog. Aerosp. Sci. 39, 511–536 (2003)

    Article  Google Scholar 

  5. Hirschel, E.H.: Viscous effects. In: Space Course 1991, vol. 12, pp. 1–35, Aachen

    Google Scholar 

  6. Bertin, J.J., Cummings, R.M.: Critical hypersonic aerothermodynamic phenomena. Ann. Rev. Fluid Mech. 38, 129–157 (2006)

    Article  MathSciNet  Google Scholar 

  7. Lu, F.K., Marren, D.E.: Advanced Hypersonic Test Facility (198). Progress in Astronautics and Aeronautics, Reston (2002)

    Google Scholar 

  8. Holden, M.S.: Design, development and calibration of the LENS facility (pp. 94–0161). AFOSR-TR (1994)

    Google Scholar 

  9. Holden, M.S., Wadhams, T.P., Candler, G.V.: A review of experimental studies in the LENS shock tunnel and expansion tunnel to examine real-gas effects in hypervelocity flows. In: 42th AIAA Aerospace Sciences Meeting and Exhibit Reno, AIAA Paper 2004-0916, NV, 5-8 Jan 2004

    Google Scholar 

  10. Holden, M.S., Chadwick, K.M., Kolly, J.M.: Hypersonic studies in the LENS facilities, AIAA 95-6040. In: 6th International Aerospace Planes and Hypersonic Technologies Conferences, Chattanooga, Tennessee, 3–7 April 1995

    Google Scholar 

  11. Stalker, R.J.: A study of the free-piston shock tunnel. AIAA J. 5, 2160–2165 (1967)

    Article  Google Scholar 

  12. Stalker, R.J., Morrison, W.R.B.: New generation of free piston shock tunnel facilities. In: Proceeding of the 17th International Symposium on Shock Tube and Waves, Bethlehem (1989)

    Google Scholar 

  13. Hornung, H.G.: The piston motion in a free-piston driver for shock tubes and tunnels, GALCIT Rep. FM88-1, 1988

    Google Scholar 

  14. Itoh, K., Ueda, S., Komuro, T., et al.: Improvement of a free piston driver for a high-enthalpy shock tunnel. Shock Waves 8, 215–233 (1998)

    Article  Google Scholar 

  15. Itoh, K., Ueda, S., Tanno, H., Komuro, T., Sato, K.: Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel. Shock Waves 12, 93–98 (2002)

    Article  Google Scholar 

  16. Bird, G.A.: A note on combustion driven tubes. Royal Aircraft Establishment, vol. 146, AGARD Report, May 1957

    Google Scholar 

  17. Yu, H.: Recent developments in detonation drivers. In: Proceedings of the Fifth National Symposium on Shock Waves and Shock tubes, Xi’an, China, Nov 1988

    Google Scholar 

  18. Yu, H., Esser, B., Lenartz, M., Grönig, H.: Gaseous detonation driver for a shock tunnel. Shock Waves 2, 245–254 (1992)

    Article  Google Scholar 

  19. Olivier, H., Jiang, Z., Yu, H., Lu, F.K.: Detonation driven shock tubes and tunnels Advanced Hypersonic Test Facilities, pp. 135–203. AIAA, USA (2002)

    Google Scholar 

  20. Jiang, Z., Yu, H., Takayama, K.: Investigation into converging gaseous detonation drivers. In: Ball, G.J., Hillier, R., Roberts, G.T. (eds.) Proceedings of ISSW22, Shock Waves, London, UK, 18–23 July 1999

    Google Scholar 

  21. Jiang, Z., Zhao, W., Wang, C., Takayama, K.: Forward-running detonation drivers for high-enthalpy shock tunnels. AIAA J. 40, 2009–2016 (2002)

    Article  Google Scholar 

  22. Zhao, W., Jiang, Z., Saito, T., Lin, J.M., Yu, H.R., Takayama, K.: Performance of a detonation driven shock tunnel. Shock waves 14(1–2), 53–59 (2005)

    Article  Google Scholar 

  23. Jiang, Z., Lin, J., Zhao, W.: Performance tests of JF-10 high-enthalpy shock tunnel with a FDC driver. J. Hypersonics 2(1), 29–35 (2011)

    Article  Google Scholar 

  24. Jiang, Z., Yu, H.: Experiments and development of long-test-duration hypervelocity detonation-driven shock tunnel (LHDst). AIAA paper 2014-1012 (2014)

    Google Scholar 

  25. Jiang, Z., Gao, Y., Zhao, W.: Performance study on detonation-driven expansion tube. AIAA paper 2009-7237 (2009)

    Google Scholar 

  26. Li, J.P., Feng, H., Jiang, Z., Yu, H.R.: Numerical computation on the tailored shock Mach numbers for a hydrogen/oxygen detonation shock tube. Acta Aerodynamica Sinica 26, 291–296 (2008)

    Google Scholar 

  27. Li, J.P., Feng, H., Jiang, Z.: Investigation into test gas contamination of shock tunnels induced by shock/boundary interactions. Acta Mechanica Sinica 40, 289–296 (2008)

    Google Scholar 

  28. Jiang, Z., Li, J.P., Zhao, W., Liu, Y.F., Yu, H.R.: Investigation into techniques for extending the test-duration of detonation-driven shock tunnel. Chinese Journal of Theoretical and Applied Mechanics 44, 824–831 (2012)

    Google Scholar 

  29. Laderman, A.L.: Shock-tube performance with area divergence at the diaphragm section. AIAA Journal 10, 1904–1906 (1967)

    Article  Google Scholar 

  30. Resler, E.L., Bloxsom, D.E.: Very High Mach Number Flows by Unsteady Flows Principles. Cornell University, Graduate School of Aeronautical Engineering, New York (1952)

    Google Scholar 

  31. Trimpi, R.L.: A preliminary theoretical study of the expansion tube: A new device for producing high-enthalpy short duration hypersonic gas flows. NASA TR-133 (1962)

    Google Scholar 

  32. Neely, A.J., Stalker, R.J., Paull, A.: High enthalpy hypervelocity flows of air and argon in an expansion tube. Aeronaut. J. 95(946), 175–186 (1991)

    Google Scholar 

  33. Sasoh, A., Morgan, R.G., et al.: High-enthalpy expansion tube experiments with gas injection. AIAA J. 38, 2253–2259 (2000)

    Article  Google Scholar 

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Acknowledgments

The author would like to acknowledge the National Natural Science Foundation of China which provides funding for this research under the projects of 10632090 and 10621202. The authors would like to thank all the members from the group of shock wave and detonation physics for their kind assistance in experiments and facility development.

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Correspondence to Zonglin Jiang .

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Jiang, Z., Yu, H. (2016). Development and Calibration of Detonation-Driven High-Enthalpy and Hypersonic Test Facilities. In: Igra, O., Seiler, F. (eds) Experimental Methods of Shock Wave Research. Shock Wave Science and Technology Reference Library, vol 9. Springer, Cham. https://doi.org/10.1007/978-3-319-23745-9_9

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  • DOI: https://doi.org/10.1007/978-3-319-23745-9_9

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