In {TAIL ~ one aspect} of the invention, a gas turbine engine is defined by a plurality of components including a housing, defining a central axis, a compressor section and {HEAD ~ a turbine section} 
In { TAIL ~ one aspect } of the invention , a gas turbine engine is defined by a plurality of components including a housing , defining a central axis , a compressor section and { HEAD ~ a turbine section }
OTH TAIL TAIL TAIL TAIL TAIL TAIL OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH OTH HEAD HEAD HEAD HEAD HEAD HEAD HEAD