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