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

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Acknowledgements

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.

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Correspondence to Jihong Zhu.

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The authors declare that they have no conflict of interest.

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Hu, S., Zhu, J. Longitudinal high incidence unsteady aerodynamic modeling for advanced combat aircraft configuration from wind tunnel data. Sci. China Inf. Sci. 60, 118201 (2017). https://doi.org/10.1007/s11432-017-9095-7

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