Air Inlet/Airframe Integration Optimization Based on the Discrete Adjoint Method

Author:

Shu Bowen,He Chengjun,Huang Jiangtao,Gao Zhenghong,Chen Xian,Deng Jun

Publisher

Springer Nature Singapore

Reference13 articles.

1. Shu, S., Guo, R.W.: Numerical analysis and experimental validation of a submerged inlet on the plane surface. Chin. J. Aeronaut. 18(3), 199–205 (2005)

2. Seddon, J., Goldsmith, F.R.: Intake Aerodynamics, 2nd edn. Blackwell science, London (1999)

3. Wenbiao, G., Zhou, Z., Xiaoping, X., et al.: S-Duct inlet optimal design and analysis. J. Propul. Technol. 35(10), 1317–1324 (2014)

4. Harrison, N.A., Anderson, J., Fleming, J.L., et al.: Active flow control of a boundary layer-ingesting serpentine inlet diffuser. J. Aircr. 50(1), 262–271 (2013)

5. Kun, W., Hexia, H., Lei, L., et al.: A new distortion evaluation method based on geometric association for arbitrary cross-sectional shape of inlet. Aerosp. Sci. Technol. 128, 1–12 (2022)

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