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2 - Shock-Wave Relations and Aerothermodynamic States

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

In this chapter, the aerodynamic fundamentals for the working principles of shock tunnels are summarized. The moving waves, including expansion waves, shock waves, and contact surfaces, are introduced as the key issues and their theories are based on the unsteady one-dimensional flows in textbooks of aerodynamics. As unsteady one-dimensional moving waves are also critical for the design and operation of shock tunnels, their theories are also selected and summarized in this chapter for book completeness and readers’ convenience.

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Publisher: Cambridge University Press
Print publication year: 2023

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References

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Paull, A. and Stalker, R. J. (1989). Experiments on an Expansion Tube with a Free Piston Driver – Phase 2. Department of Mechanical Engineering Report, The University of Queensland.Google Scholar
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