A gas turbine engine in {TAIL ~ accordance} 10 wherein said flow path further comprises an apex defined within {HEAD ~ said first portion} 
A gas turbine engine in { TAIL ~ accordance } 10 wherein said flow path further comprises an apex defined within { HEAD ~ said first portion }
OTH OTH OTH OTH OTH TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD