Numerical Investigation on Supersonic Airflow Around Tangent Ogive Wedge of Varying Fineness Ratio
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42423-024-00151-5.pdf
Reference15 articles.
1. Chen YC, Gao XB, Gao M (2018) Investigation of the aerodynamic parameters simulation method of a guided rocket. SIMULATION 94(6):477–491. https://doi.org/10.1177/0037549717737854
2. Hirschel EH (2015) Basics of aerothermodynamics, 2nd edn. Springer International Publishing, Cham, p 446
3. Urazbakhtin FA, Kharinova YY, Urazbakhtin VF (2014) A mathematical model of heat shielding for a nose cone taking into account critical flight situations. Russ Aeronaut 57:100–106. https://doi.org/10.3103/S1068799814010140
4. Chalia S, Bharti MK (2016) Mathematical modeling of ogive forebodies and nose cones. Int Res J Eng Technol 3(3):744–747
5. Amini Y, Emdad H, Akramian K, Bordbar F (2012) Investigation of the common nose cone shapes in different gas mixtures in high Knudsen numbers. Sci Iran 19(6):1511–1518. https://doi.org/10.1016/j.scient.2012.10.029
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