| Citation: | PENG Wei, JIANG Pei-xue. Investigation of supersonic film cooling in flat and convex channels[J]. Journal of Aerospace Power, 2008, 23(3): 406-409. |
| [1] |
Kanda T,Masuya G,Ono F,et al.Effect of film cooling/ regenerative cooling on scramjet engine performances[J].Journal of Propulsion and Power,1994,10(5):618-624.
|
| [2] |
Juhany K A,Hunt M L.Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction[J].AIAA Journal,1994,32(3):578-585.
|
| [3] |
O' Connor J P,Hail-Sheikh A.Numerical study of film cooling in supersonic flow[J].AIAA Journal,1992,30 (10):2426-2433.
|
| [4] |
Takita K,Masuya G.Effects of combustion and shock impingement on supersonic film cooling by hydrogen[J].AIAA Journal,2000,38(10):1899-1906.
|
| [5] |
Juhany K A,Hunt M L,Sivo J.Influence of injectant Mach number and temperature on supersonic film cooling[J].Journal of Thermophysics and Heat Transfer,1994,8(1):59-67.
|
| [6] |
Goldstein R J,Eckert E R G,Tson F K,et al.Film cooling with air and helium injection through a rearward-facing slot into a supersonic air flow[J].AIAA Journal,1966,4(6):981-985.
|
| [7] |
Kanda T,Ono F,Takahashi M,et al.Experimental studies of supersonic film cooling with shock wave interaction[J].AIAA Journal,1996,34(2),265-271.
|