Aerodynamic Modeling and Analysis of Receiver Under the Disturbance of Tanker’s Wake Flow

Author:

Wangyi Zhou,Xiheng Zang,Lei Qiao,Chao Jiang,Xueyao Zhu

Publisher

Springer Nature Singapore

Reference14 articles.

1. Yuyan, H.: Development of foreign aerial refueling technology. Flight Dynam. 12(4), 14–22 (1994). (in Chinese)

2. Li, H., Huang, A., Jia, R.: Model and simulation of wake interference in air-to-aerial refueling flight simulation. J. Syst. Simulat., 20(4), 1020–1023 (2008) (in Chinese)

3. Jewell, W., Stapleford, R.: Mathematical models used to simulate aircraft encounters with wake vortice. NASA-TR-1035–4 (1975)

4. Rossow, V.J., Corsiglia, V.R., Schwind, R.G.: Velocity and rolling-moment measurements in the wake of a swept-wing model in the 40-by-80-foot wind tunnel. NASA-TM-X-62414 (1975)

5. Bloy, A.W., Lamont, P.J., Abu-Assaf, H.A.: The lateral dynamic stability and control of a large receiver aircraft during air-to-aerial refueling. Aeronautical J. 90(896), 237–243 (1986)

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