CHEN D H, LIN J, GUO D P, et al.Technical ways to solve high speed key aerodynamic problems of large air transporters[J].Experiments and Measurements in Fluid Mechanics, 2003, 18(2):1-5.(in Chinese)

WANG F X, et al.High speed wind tunnel test[M].Beijing:National Defense Industry Press, 2003.(in Chinese)

HUANG Y, DONG L X, ZHAO K C, et al.On the correlation of force test results of a tactical missile calibration model in five different windtunnels[J].Experiments and Measurements in Fluid Mechanics, 2002, 16(2):16-20.(in Chinese)

CHEN D H, LIU D W, XU X, et al.Investigation on factors influencing high speed wind tunnel data for large airplane[C].8th National Fluid Dynamics Conference, 2014.(in Chinese)

FAN J C, CHEN D H, PENG Y, et al.Research on force test technique of UAV model with large aspect ratio in high speed wind tunnel[J].Journal of Experiments in Fluid Mechanics, 2007, 21(3):62-65.(in Chinese)

CHEN D H, YIN L P, WU W H, et al.The test technique for aircraft with high aspect ratio in the 2.4 meter transonic windtunnel[J].Acta Aerodynamica Sinica, 2009, 27(5):542-546.(in Chinese)

WANG R, WU J, GUO Q, et al.Research on the affecting factors of test quality and improvement methods in 2.4 m transonic wind tunnel[J].Journal of Experiments in Fluid Mechanics, 2012, 26(1):37-41.(in Chinese)

GREGORY M G, MELISSA B R, SCOTT L G, et al.Experimental Investigation of the DLR-F6 Transport Configuration in the National Transonic Facility[C].26th AIAA Applied Aerodynamics Conference, 2008.

MELISSA B R, CRAIG A H, GREGORY M G.Support system effects on the DLR-F6 transport configuration in the national transonic facility[C].27th AIAA Applied Aero-dynamics Conference, 2009.

RALF R, MARTIN S, JEAN L G, et al.Experimental investigation of the wing-body juncture flow on the DLR-F6 configuration in the ONERA S2MA facility[C].27th AIAA Applied Aerodynamics Conference, 2009.

ALPHEUS W BURNER, WILLIAM K GOAD, EDWARD A MASSEY, et al.Wing deformation measurements of the DLR-F6 transport configuration in the national transonic facility[C].26th AIAA Applied Aerodynamics Conference, 2008.

THORSTEN L, PHILIPP P G, JEAN L G, et al.Going for experimental and numerical unsteady wake analyses combined with wall interference assessment by using the NASA CRM model in ETW[C].51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013.

WANG Y T, WANG G X, ZHANG Y L.Drag of DLR-F6 wing-body configuration[J].Chinese Journal of Computational Physics, 2008, 25(2):145-150.(in Chinese)

ANTONY J S, JOHN C V, NEAL A H, et al.Drag prediction for the DLR-F6 wing body and DPW wing using CFL3D and OVERFLOW on an Overset Mesh[C].45th AIAA Aerospace Sciences Meeting and Exhibit, 2007.

CHEN D H, WANG W X, WANG J J, et al.Investigation on flow-field debugging for 2.4 m transonic wind tunnel[J].Acta Aerodynamica Sinica, 2004, 22(3):279-282.(in Chinese)

ZHAN P G, LUO Y P.Primary research on the standard system of air vehicle calibration models used in wind tunnel test[J].Standard Science, 2011, 11(2):28-31.(in Chinese)

YU Y G, ZHOU Z, HUANG J T, et al.Aerodynamic design of a standard model CHN-T1 for single-aisle passenger aircraft[J].Acta Aerodynamica Sinica, 2018, 36(03):505-513.(in Chinese)

LI W, MENG D H, WANG Y T, et al.Numerical simulation of CHNG-T1 model with TRIP3.0[J].Acta Aerodynamica Sinica, 2019, 37(2):272-279.(in Chinese)

路波, 等.高速风洞测力试验数据处理方法[D].北京: 国防工业出版社, 2014.

CHENG H M.Interference and correction on wind tunnel testing[M].Beijing:National Defense Industry Press, 2003.(in Chinese)

LI Q, LIU D W, CHEN D H, et al.Study on the support Interference of vane suspension support system in high speed wind tunnels[J].Journal of Experiments in Fluid Mechanics, 2017, 31(1):100-108.(in Chinese)

HE B H, LI W, LIU D W, Technology Research of Complicated Configuration Oil-flow Experimentation of High Speed Wind Tunnel[R].Mianyang: CARDC, 2017.(in Chinese)