Aerodynamic Layout Designs Using of Microflaps for Flow Control of a Supersonic Finned Projectile
In this paper, the flow control system consists of some small microflaps located between the rear fins of the projectile. These microflaps can alter the flow field in the finned region of the projectile resulting in asymmetric pressure distribution and thus producing control forces and moments, furt...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2019-04-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2019/02/jnwpu2019372p344/jnwpu2019372p344.html |