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《Aerospace Science and Technology》2007,11(2-3):202-210
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《Aerospace Science and Technology》2006,10(6):484-494
This paper presents RANS simulations of the low-Reynolds-number flow past an SD7003 airfoil at , where transition takes place across a laminar separation bubble. The transition prediction procedure using an approximate envelope method as well as a linear stability solver is discussed. The numerical results are validated against PIV- and force measurements obtained in several wind- and watertunnels and are also compared to XFOIL results. Good agreement is found within the operational range of the airfoil. 相似文献
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Scale effect of fuel regression rate in hybrid rocket motor 总被引:1,自引:0,他引:1
Guobiao Cai Peng Zeng Xintian Li Hui Tian Nanjia Yu 《Aerospace Science and Technology》2013,24(1):141-146