The invention relates to {TAIL ~ a static shroud} for a gas turbine engine made of a sheet of {HEAD ~ metal} bent to form a contiguous shroud body having a substantially uniform sheet thickness and a uniform axial profile 
The invention relates to { TAIL ~ a static shroud } for a gas turbine engine made of a sheet of { HEAD ~ metal } bent to form a contiguous shroud body having a substantially uniform sheet thickness and a uniform axial profile
OTH OTH OTH OTH TAIL TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH