Recent investigations of shock wave effects and interactions

被引:60
作者
Ligrani, P. M. [1 ,2 ]
McNabb, E. S. [1 ,2 ]
Collopy, H. [1 ,2 ]
Anderson, M. [1 ,2 ]
Marko, S. M. [1 ,2 ]
机构
[1] Prop Res Ctr, Dept Mech & Aerosp Engn, Olin B King Technol Hall S236,5000 Technol Dr, Huntsville, AL 35899 USA
[2] Univ Alabama Huntsville, Huntsville, AL 35899 USA
关键词
Shock wave; Supersonic flow; Unsteady flow; Supersonic test sections; Thermal transport; Heat transfer; Shock wave control; TURBULENT-BOUNDARY-LAYER; LOW-FREQUENCY UNSTEADINESS; ROTOR HEAT-TRANSFER; BLADE TIP CAVITY; TRANSONIC TURBINE; PASSIVE CONTROL; SEPARATION; PERFORMANCE; FLOW; OPTIMIZATION;
D O I
10.1186/s42774-020-0028-1
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Despite over fifty years of research on shock wave boundary layer effects and interactions, many related technical issues continue to be controversial and debated. The present survey provides an overview of the present state of knowledge on such effects and interactions, including discussions of: (i) general features of shock wave interactions, (ii) test section configurations for investigation of shock wave boundary layer interactions, (iii) origins and sources of unsteadiness associated with the interaction region, (iv) interactions which included thermal transport and convective heat transfer, and (v) shock wave interaction control investigations. Of particular interest are origins and sources of low-frequency, large-scale shock wave unsteadiness, flow physics of shock wave boundary layer interactions, and overall structure of different types of interactions. Information is also provided in regard to shock wave investigations, where heat transfer and thermal transport were important. Also considered are investigations of shock wave interaction control strategies, which overall, indicate that no single shock wave control strategy is available, which may be successfully applied to different shock wave arrangements, over a wide range of Mach numbers. Overall, the survey highlights the need for additional understanding of fundamental transport mechanisms, as related to shock waves, which are applicable to turbomachinery, aerospace, and aeronautical academic disciplines.
引用
收藏
页数:23
相关论文
共 117 条
[1]   COMPARISON OF TIME-RESOLVED TURBINE ROTOR BLADE HEAT-TRANSFER MEASUREMENTS AND NUMERICAL-CALCULATIONS [J].
ABHARI, RS ;
GUENETTE, GR ;
EPSTEIN, AH ;
GILES, MB .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (04) :818-827
[2]  
Anderson B., 2006, 3rd aiaa flow control conference, P3197, DOI DOI 10.2514/2006-3197
[3]  
Anderson BH., 2006, 214373 NASA TM
[4]  
[Anonymous], 1975, 3 D SHOCK WAVE TURBU
[5]  
Anto K, 2013, PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3C
[6]   An Experimental and Numerical Study on the Aerothermal Characteristics of a Ribbed Transonic Squealer-Tip Turbine Blade With Purge Flow [J].
Arisi, A. ;
Phillips, J. ;
Ng, W. F. ;
Xue, S. ;
Moon, H. K. ;
Zhang, L. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2016, 138 (10)
[7]  
Ashill P.R., 1992, 1 EUR FOR LAM FLOW T, P175
[8]   UNSTEADY AERODYNAMIC AND HEAT-TRANSFER PROCESSES IN A TRANSONIC TURBINE STAGE [J].
ASHWORTH, DA ;
LAGRAFF, JE ;
SCHULTZ, DL ;
GRINDROD, KJ .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1985, 107 (04) :1022-1030
[9]   Unsteady Effects on Transonic Turbine Blade-Tip Heat Transfer [J].
Atkins, Nicholas R. ;
Thorpe, Steven J. ;
Ainsworth, Roger W. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (06)
[10]   Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions [J].
Babinsky, H. ;
Li, Y. ;
Ford, C. W. Pitt .
AIAA JOURNAL, 2009, 47 (03) :668-675