The method 8 wherein {HEAD ~ the cooling air} is supplied to {TAIL ~ a first annular cavity} formed by said annular seal structure and then to a second annular cavity within said aft end of said combustor liner 
is supplied to
The method 8 wherein { HEAD ~ the cooling air } is supplied to { TAIL ~ a first annular cavity } formed by said annular seal structure and then to a second annular cavity within said aft end of said combustor liner
OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD REL REL REL TAIL TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH