“…One of the most promising heat recuperators used in aero-engines is the double-U-shaped tube bundle heat exchanger (Min, Jeong, Ma, & Kim, 2009). Although extensive investigations have been carried out concerning the flow development and overall heat transfer through the tube bundle geometry (Horvat, Leskovar, & Mavko, 2006;Ranut, Janiga, Nobile, & Dominique, 2014;F. M. Wang, Zhang, & Wang, 2007), limited work has been performed on the flow and overall heat transfer through heat exchangers embedded inside an aero-engine exhaust nozzle, where the external flow passing through the tube bundle is more complicated due to various angles of attack.…”