Hypersonic flow past a spherically blunted nose cone: a computational study-Reference-Cited by-同舟云学术

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Hypersonic flow past a spherically blunted nose cone: a computational study

Published:2020 Issue:2 Volume:20 Page:105
ISSN:1468-4349
Container-title:Progress in Computational Fluid Dynamics, An International Journal
language:en
Short-container-title:PCFD

Author:

Narayan Ashish,Narayanan S.,Kumar Rakesh,Kumar Chintoo Sudhiesh,Jagadeesh Gopalan

Publisher

Inderscience Publishers

Subject

Computer Science Applications,Condensed Matter Physics

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Reducing aerodynamic drag and heat generation in parabolic nose cones using single and double-disc tapered spikes;Numerical Heat Transfer, Part B: Fundamentals;2024-08-05

2. Study of shock shapes around blunted conical bodies in hypersonic flow;Journal of Physics: Conference Series;2024-08-01

3. Numerical Investigation of Aerodynamic Characteristics on a Blunt Cone Model at Various Angles of Attack under Hypersonic Flow Regimes;SAE Technical Paper Series;2024-06-01

4. Heat flux and aerodynamics drag reduction of a hypersonic flow with the different tips of the taper spike design parabolic nose cone;Numerical Heat Transfer, Part A: Applications;2024-01-11

5. Computational fluid dynamics analysis on drag from structural joint bolts of RX-450 sounding rocket;AIP Conference Proceedings;2024

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