High-Pressure Shock Tunnel Experiments and CFD Calculations on Spike-Tipped Blunt Bodies-Reference-Cited by-同舟云学术

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High-Pressure Shock Tunnel Experiments and CFD Calculations on Spike-Tipped Blunt Bodies

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Srulijes Julio¹,Gnemmi Patrick¹,Runne Kay²,Seiler Friedrich¹

Affiliation:

1. French-German Research Institute of Saint-Louis

2. EADS Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2918

Reference20 articles.

Cited by 13 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

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2. Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-12

3. Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds;Journal of Aerospace Engineering;2020-11

4. Drag of a Spiked Body in Chemically Reacting Hypersonic Flow;Journal of Spacecraft and Rockets;2020-09

5. Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows;International Journal of Heat and Mass Transfer;2018-11

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