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).
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
Bertin, J.J.: Hypersonic Aerothermodynamics. AIAA Education Series, Washington DC (1994)
Park, C.: Nonequilibrium Hypersonic Aerothermodynamics. Wiley, New York (1990)
Anderson, J.D.: Hypersonic and High Temperature Gas Dynamics. McGraw-Hill Book Company, New York (1989)
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)
Hirschel, E.H.: Viscous effects. In: Space Course 1991, vol. 12, pp. 1–35, Aachen
Bertin, J.J., Cummings, R.M.: Critical hypersonic aerothermodynamic phenomena. Ann. Rev. Fluid Mech. 38, 129–157 (2006)
Lu, F.K., Marren, D.E.: Advanced Hypersonic Test Facility (198). Progress in Astronautics and Aeronautics, Reston (2002)
Holden, M.S.: Design, development and calibration of the LENS facility (pp. 94–0161). AFOSR-TR (1994)
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
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
Stalker, R.J.: A study of the free-piston shock tunnel. AIAA J. 5, 2160–2165 (1967)
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)
Hornung, H.G.: The piston motion in a free-piston driver for shock tubes and tunnels, GALCIT Rep. FM88-1, 1988
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)
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)
Bird, G.A.: A note on combustion driven tubes. Royal Aircraft Establishment, vol. 146, AGARD Report, May 1957
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
Yu, H., Esser, B., Lenartz, M., Grönig, H.: Gaseous detonation driver for a shock tunnel. Shock Waves 2, 245–254 (1992)
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)
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
Jiang, Z., Zhao, W., Wang, C., Takayama, K.: Forward-running detonation drivers for high-enthalpy shock tunnels. AIAA J. 40, 2009–2016 (2002)
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)
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)
Jiang, Z., Yu, H.: Experiments and development of long-test-duration hypervelocity detonation-driven shock tunnel (LHDst). AIAA paper 2014-1012 (2014)
Jiang, Z., Gao, Y., Zhao, W.: Performance study on detonation-driven expansion tube. AIAA paper 2009-7237 (2009)
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)
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)
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)
Laderman, A.L.: Shock-tube performance with area divergence at the diaphragm section. AIAA Journal 10, 1904–1906 (1967)
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)
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)
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)
Sasoh, A., Morgan, R.G., et al.: High-enthalpy expansion tube experiments with gas injection. AIAA J. 38, 2253–2259 (2000)
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.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2016 Springer International Publishing Switzerland
About this chapter
Cite this chapter
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
Download citation
DOI: https://doi.org/10.1007/978-3-319-23745-9_9
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-23744-2
Online ISBN: 978-3-319-23745-9
eBook Packages: EngineeringEngineering (R0)