Abstract: An exhaust system for a gas turbine engine is provided. The exhaust system includes an exhaust diffuser having a diffuser axis. The exhaust diffuser includes an outer diffuser wall. The exhaust diffuser also includes an inner diffuser wall. The exhaust diffuser further includes a diffuser inlet formed by the first and second upstream ends of the outer diffuser wall and the inner diffuser wall. The exhaust diffuser includes a diffuser exit. The exhaust system also includes an exhaust collector coupled with the exhaust diffuser and adapted to collect and redirect exhaust gases in a radial direction. The exhaust collector includes a circumferential wall. The exhaust collector also includes a forward wall. The exhaust collector further includes an aft wall, wherein the aft wall is angled with respect to the diffuser axis. The exhaust collector includes a splitter disposed between the forward wall and the aft wall of the exhaust collector.