Abstract
Convective heat-transfer-rates have been measured on the surface of a cylinder using platinum thin film gauges in a diaphragm-less shock tube. The measured values are compared with the simulated results of two numerical codes at different flow Mach and Reynolds numbers. The measured and simulated results give an insight into the transient flow fields around the model in the shock tube and are a valuable means to complement the numerical and experimental techniques used in the study.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
W.J. Cook, E. J. Felderman: AIAA J. 4, 561 (1966)
D. Hermann, F. P. Wesslau, G. Adomeit: In: Proc. ISSW 16, pp. 821, Aachen (1987)
A. Roshko: J. Fluid Mech. 10, 345 (1961)
M. Sun: Numerical and experimental studies of shock wave interaction with bodies. Ph. D. Thesis, Tohoku University, Japan (1999)
M. Sun, K. Takayama: J. Compt. Phys. 150, 143 (1999)
M. Sun, K. Takayama: J. Compt. Phys. 189, 305 (2003)
R. J. Vidal: CAL Rep. WADC TN 56-315 (1956)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Kuribayashi, T., Saito, T., Menezes, V., Sun, M., Jagadeesh, G., Takayama, K. (2005). Heat transfer measurement and its application to CFD code evaluation. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_19
Download citation
DOI: https://doi.org/10.1007/978-3-540-27009-6_19
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-22497-6
Online ISBN: 978-3-540-27009-6
eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)