[1] LU J,GAO F.Process modeling based on process similarity[J].Industrial & Engineering Chemistry Research,2008,47(6):1967-1974.
[2] LU J,YAO Y,GAO F.Model migration for development of a new process model[J].Industrial & Engineering Chemistry Research,2008,48(21):9603-9610.
[3] LU J,GAO F.Model migration with inclusive similarity for development of a new process model[J].Industrial & Engineering Chemistry Research,2008,47(23):9508-9516.
[4] COX R N,CRABTREE L F.Elements of hypersonic aerodynamics[M]. London:The English Universities Press LTD.,1965:18-55.
[5] HAYES W.Hypersonic flow theory[M].New York:Academic Press,2012:36-67.
[6] 瞿章华,刘伟,曾明,等.高超声速空气动力学[M].长沙:国防科技大学出版社,2001:40-47.QU Z H,LIU W,ZENG M,et al.Hypersonic aerodynamics[M].Changsha:National University of Defense Technology Publishing,2001:40-47(in Chinese).
[7] NEICE S E,EHRET D M.Similarity laws for slender bodies of revolution in hypersonic flow[J].Journal of the Aeronautical Science,1951,18(8):527-538.
[8] VANDYKE M D.The combined supersonic-hypersonic similarity rule[J].Journal of the Aeronautical Sciences,2012,18(7):499-500.
[9] HAMAKER F M,NEICE S E,EGGERS JR A J.The similarity law for hypersonic flow about slender three-dimensional shapes:NO.NACA-TN-2443[R].Washington,D.C.:National Aeronautics and Space Administration Moffett Field Caames Research Center,1951:1-22.
[10] 张涵信.高超声速空气动力学[M].长沙:国防科技大学出版社,1982:32-50.ZHANG H X.Hypersonic aerodynamics[M].Changsha:National University of Defense Technology Publishing,1982:32-50(in Chinese).
[11] ANDERSON J D.Hypersonic and high temperature gas dynamics[M].New York:Mc Graw-Hill Book Company,1989:2-12.
[12] SCHLICHTING H,GERSTEN K.Boundary-layer theory[M].London:Springer,2000:23-57.
[13] MORGAN B,DURAIAMY K,NGUYEN N,et al.Flow physics and RANS modeling of oblique shock/turbulent boundary layer interaction[J].Journal of Fluid Mechanics,2013,729:231-284.
[14] JAUNET V,DEBIEVE J F,DUPONT P.Length scales and time scales of a heated shock-wave/boundary-layer interaction[J].AIAA Journal,2014,52(11):2524-2532.
[15] FEDOROV A V,MALMUTH N D.Application of similarity in hypersonic transition prediction[J].AIAA Journal,1995,33(8):1523-1525.
[16] HERMES V,OLIVIER H.On the transformation of the angle of attack for supersonic similarity rules[J].Journal of Aircraft,2013,50(1):302-304.
[17] 叶友达.高空高速飞行器气动特性研究[J].力学进展,2009,39(4):387-397.YE Y D.Study on aerodynamic characteristics of high velocity vehicle flying at high altitede[J].Advances in Mechanics,2009,39(4):387-397. |