Skip to main content Accessibility help

We use cookies to distinguish you from other users and to provide you with a better experience on our websites. Close this message to accept cookies or find out how to manage your cookie settings.

Close cookie message
×
Hostname: page-component-848d4c4894-m9kch Total loading time: 0 Render date: 2024-05-28T19:36:53.430Z Has data issue: false hasContentIssue false
This chapter is part of a book that is no longer available to purchase from Cambridge Core

6 - Theory and Methods for Long-Test-Duration Shock Tunnels

Zonglin Jiang  and
Randy S. M. Chue
Zonglin Jiang
Affiliation:
Chinese Academy of Sciences, Beijing
Randy S. M. Chue
Affiliation:
Nanyang Technological University, Singapore
Get access

Summary

Based on detonation-driven shock tunnels, key issues that play important roles in extending the test time are introduced in this chapter, and the corresponding solutions are proposed, evaluated, and discussed in detail, including the tailored-interface condition, the shock–boundary-layer interaction at the end of the driven section, and the precursor shock damping in the vacuum tank. The research work on these issues was carried out to find out the flow physics and application methods to improve the high-enthalpy shock tunnel for meeting the test time requirement for supersonic combustion and scramjet engine experiments. With application of the aforementioned theories and methods to the high-enthalpy shock tunnel, a large-scale detonation-driven hypersonic flight-duplicated shock tunnel (the JF-12 shock tunnel) was successfully developed, which can provide test times of more than 100 microseconds and is capable of duplicating hypersonic flight conditions for Mach numbers of 5–9 at altitudes of 25–50 km.

Keywords

detonation-driventest timehypersonic flight conditionduplicationtailored interface
Type
Chapter
Information
Theories and Technologies of Hypervelocity Shock Tunnels , pp. 165 - 191
Publisher: Cambridge University Press
Print publication year: 2023

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Anderson, J. D. (1989). Hypersonic and High Temperature Gas Dynamics. New York: McGraw-Hill Book Company.Google Scholar
Bertin, J. J. (1994). Hypersonic Aerothermodynamics. Washington, DC: AIAA Education Series.Google Scholar
Bertin, J. J. and Cummings, R. M. (2003). Fifty Years of Hypersonics: Where We’ve Been, Where We’re Going. Progress in Aerospace Sciences, 39(6–7), 511–536.Google Scholar
Bertin, J. J. and Cummings, R. M. (2006). Critical Hypersonic Aerothermodynamic Phenomena. Annual Review of Fluid Mechanics, 38, 129–157.Google Scholar
Burtschell, Y. and Cardoso, M. (2001). Numerical Analysis of Reducing Driver Gas Contamination in Impulse Shock Tunnels. AIAA Journal, 39(12), 2357–2365.Google Scholar
Chue, R. S. M. and Eitelberg, G. (1998). Studies of the Transient Flows in High Enthalpy Shock Tunnels. Experiments in Fluid, 25, 474–486.Google Scholar
Davies, L. and Wilson, J. L. (1969). Influence of a Reflected Shock and Boundary Interaction on Shock Tube Flows, Physics of Fluid, 12(5), S37–S43.Google Scholar
Jiang, Z. and Yu, H. (2014). Experiments and Development of Long-Test-Duration Hypervelocity Detonation-driven Shock Tunnel (LHDst). AIAA Paper 2014–1012 (Invited Lecture).Google Scholar
Jiang, Z. and Yu, H. (2017). Theories and Technologies for Duplicating Hypersonic Flight Conditions for Ground Testing. National Science Review, 4(3), 290–296.Google Scholar
Jiang, Z., Hu, Z., Wang, Y., and Han, G. (2020a). Advances in Critical Technologies for Hypersonic and High-enthalpy Wind Tunnel. Chinese Journal of Aeronautics, 33(12), 3027–3038.Google Scholar
Jiang, Z., Li, J., Hu, Z., Liu, Y., and Yu, H. (2020b). On Theory and Methods for Advanced Detonation-driven Hypervelocity Shock Tunnels. National Science Review, 7(7), 1198–1207.Google Scholar
Jiang, Z. and Teng, H. (2022). Gaseous Detonation Physics and Its Universal Framework Theory, Singapore: Springer.Google Scholar
Jiang, Z., Wu, B., Gao, Y., Zhao, W., and Hu, Z. (2015). Development of the Detonation-driven Expansion Tube for Orbital Speed Experiments. Science China, 58(4), 695–700.Google Scholar
Jiang, Z., Zhang, Z., Liu, Y., Wan, C., and Luo, C. (2021) The Criteria for Hypersonic Airbreathing Propulsion and Its Experimental Verification. Chinese Journal of Aeronautics, 34(3), 94–104.Google Scholar
Jiang, Z., Zhao, W., Wang, C., and Takayama, K. (2002). Forward-running Detonation Drivers for High-enthalpy Shock Tunnels. AIAA Journal, 40(10), 2009–2016.Google Scholar
Lee, J. (2008). The Detonation Phenomenon. New York: Cambridge University Press.Google Scholar
Li, J., Feng, H., Jiang, Z., and Yu, Y. (2008a). Numerical Computation on the Tailored Shock Mach Numbers for a Hydrogen-oxygen Detonation Shock Tube. Acta Aerodynamica Sinica, 26(3), 291–296 (In Chinese).Google Scholar
Li, J., Feng, H., and Jiang, Z. (2008b). Gas Contamination Induced by the Interaction of Shock/Boundary Layer in Shock Tunnel. Chinese Journal of Theoretical and Applied Mechanics, 40(3), 289–296 (In Chinese).Google Scholar
Lu, F. K. and Marren, D. E. (2002). Advanced Hypersonic Test Facility, Progress in Astronautics and Aeronautics. Vol. 198, Reston, VA: AIAA.Google Scholar
Mark, H. (1958). The Interaction of a Reflected Shock with the Boundary Layer in a Shock Tube. NACA TM No. 20050019632.Google Scholar
Olivier, H., Jiang, Z., Yu, H., and Lu, F. K. (2002). Detonation-driven Shock Tubes and Tunnels, Advanced Hypersonic Test Facilities. Reston, VA: AIAA, 135–203.Google Scholar
Ozer, I. and Friedrich, S. (2016). Experimental Methods of Shock Wave Research. Heidelberg, New York, Dordrecht, London: Springer.Google Scholar
Park, C. (1990). Nonequilibrium Hypersonic Aerothermodynamics. New York: Wiley.Google Scholar
Wilson, G. J. (1993). Time-Dependent Simulation of Reflected-Shock/Boundary Layer Interaction. AISAS-93-0480.Google Scholar
Yuan, C. and Jiang, Z. (2021). Experimental Investigation of Hypersonic Flight-duplicated Shock Tunnel Characteristics. Acta Mechanica Sinica, 37(3), 420–431Google Scholar
Zhao, W. (2005). Performance of a Detonation Driven Shock Tunnel. Shock Waves, 14, 53–59.Google Scholar

Save book to Kindle

To save this book to your Kindle, first ensure coreplatform@cambridge.org is added to your Approved Personal Document E-mail List under your Personal Document Settings on the Manage Your Content and Devices page of your Amazon account. Then enter the ‘name’ part of your Kindle email address below. Find out more about saving to your Kindle.

Note you can select to save to either the @free.kindle.com or @kindle.com variations. ‘@free.kindle.com’ emails are free but can only be saved to your device when it is connected to wi-fi. ‘@kindle.com’ emails can be delivered even when you are not connected to wi-fi, but note that service fees apply.

Find out more about the Kindle Personal Document Service.

Available formats
×

Save book to Dropbox

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Dropbox.

Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

Available formats
×