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