1 장성하, "슬롯 형상이 경사충격파 간섭유동의 피동제어에 미치는 영향에 관한 연구" 한국항공우주학회 34 (34): 18-24, 2006
2 and Mabey, "″Passive Shock-Wave/Boundary-Layer Control on a Wall-Mounted Model" 275-278, 1987
3 Sun, "″A Modified Wall Wake Velocity Profile for Turbulent Compressible Boundary Layers ″ Journal of Aircraft" 1973
4 ″Shock Wave/Turbulent Boundary Layer Interaction, "″ Progress in Aerospace Sciences" 209-280, 1985
5 Bur, R, "Study of Passive Control in a Transonic Shock Wave/Boundary-Layer Interaction" 36 (36): 394-400, 1998
6 Lee, Y, "Skin Friction Measurements for Recirculating Normal Shock Boundary Layer Interaction Control" 42 (42): 806-814, 2004
7 Mcllwain, S. T, "Simulation of an Aeroelastic Control System for Shock/Boundary-Layer Interactions" 2001
8 Jaiman, R. K, "Simulation of Normal Shock Wave/ Boundary-Layer Interaction Control Using Mesoflaps" 20 (20): 344-352, 2004
9 Wood, B, "Simulation of Aeroelastic Mesoflaps for Shock/Boundary-Layer Interaction" 16 (16): 1127-1144, 2002
10 Settles, "Progress in Astronautics and Aeronautics" 104 : 297-379, 1986
1 장성하, "슬롯 형상이 경사충격파 간섭유동의 피동제어에 미치는 영향에 관한 연구" 한국항공우주학회 34 (34): 18-24, 2006
2 and Mabey, "″Passive Shock-Wave/Boundary-Layer Control on a Wall-Mounted Model" 275-278, 1987
3 Sun, "″A Modified Wall Wake Velocity Profile for Turbulent Compressible Boundary Layers ″ Journal of Aircraft" 1973
4 ″Shock Wave/Turbulent Boundary Layer Interaction, "″ Progress in Aerospace Sciences" 209-280, 1985
5 Bur, R, "Study of Passive Control in a Transonic Shock Wave/Boundary-Layer Interaction" 36 (36): 394-400, 1998
6 Lee, Y, "Skin Friction Measurements for Recirculating Normal Shock Boundary Layer Interaction Control" 42 (42): 806-814, 2004
7 Mcllwain, S. T, "Simulation of an Aeroelastic Control System for Shock/Boundary-Layer Interactions" 2001
8 Jaiman, R. K, "Simulation of Normal Shock Wave/ Boundary-Layer Interaction Control Using Mesoflaps" 20 (20): 344-352, 2004
9 Wood, B, "Simulation of Aeroelastic Mesoflaps for Shock/Boundary-Layer Interaction" 16 (16): 1127-1144, 2002
10 Settles, "Progress in Astronautics and Aeronautics" 104 : 297-379, 1986