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SCIENCE CHINA Information Sciences, Volume 60, Issue 11: 118201(2017) https://doi.org/10.1007/s11432-017-9095-7

Longitudinal high incidence unsteady aerodynamic modeling for advanced combat aircraft configuration from wind tunnel data

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  • ReceivedMar 23, 2017
  • AcceptedApr 20, 2017
  • PublishedAug 17, 2017

Abstract

There is no abstract available for this article.


Acknowledgment

The advanced combat aircraft configuration model was made and corresponding wind tunnel tests were conducted by AVIC Aerodynamics Research Institute. The authors thank their great contributions to this work.


Supplement

Appendixes A and B.


References

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