Abstract
Force measurement of a standard model HB-2 was performed in high enthalpy shock tunnel HIEST to study its aerodynamic characteristics. The force measurement results were compared with that obtained in conventional 1.27m hypersonic wind tunnel HWT1. The comparison showed that HIEST results agreed well with that of HWT1 in case of low enthalpy condition. The real gas effect on aerodynamic characteristics was also studied in case of high enthalpy condition.
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References
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© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg
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Sato, K. et al. (2005). An experimental study on aerodynamic characteristics of standard model HB-2 in high enthalpy shock tunnel HIEST. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_38
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DOI: https://doi.org/10.1007/978-3-540-27009-6_38
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Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-22497-6
Online ISBN: 978-3-540-27009-6
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