Abstract
Aeroballistic range is a great facility for measuring a near field pressure around a supersonic free flight model. Commonly-used wind tunnel experiments enable to measure the pressure data under well controlled attitude conditions. However the obtained data are influenced by a sting and boundary layer.
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References
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Imaizumi, T., Toyoda, A., Sasoh, A. (2015). Gasdynamics/Mechanical Hybrid Sabot Separation Method Rectangular-Bore Ballistic Range. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 1. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16835-7_60
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DOI: https://doi.org/10.1007/978-3-319-16835-7_60
Publisher Name: Springer, Cham
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Online ISBN: 978-3-319-16835-7
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