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2.4米跨声速风洞条带悬挂支撑试验技术研究

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: 66-70.[ 0 ] 贺德馨.风洞天平[ M ] .北京:国防工业出版社2001: 189-1 9 8 .[ 1 ] 陈德华,刘大伟,尹陆平,等.2. 4 m跨声速风洞多功能支撑系统试验技术研究[ ] .实验流体力学,2013, 27(3): 98-112.[ 2 ] 张涵信.关于C F D高精度保真的数值模拟研究[ ] .空气动力学学报,2016, 34(1) : 1-4.[13] Lynch F T. The crucial role of wall interference, support inter-ference, and flow field measurments in the development of ad-vanced aircraft configurations[R]. A G A R D , 1993.[14] Masataka K. Wall and support interference corrections of N A S A c o m m o n research model wind tunnel tests in J A X A [ R ] . A I A A 2013-0963.[15] Steinbach D. Calculation of support interference on the aerody-namic coeffcients for a wind tunnel calibration model[J]. The Aeronautical Journal, 1991,10(2): 1564-1571.[ 6 ]周伟江,马汉东,白鹏.腹支撑对飞行器高超声速试验结果影响的数值计算[ ] .宇航学报,2003, 24(6): 616-620.

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