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