Abstract: A horizontal inlet section of a jet engine diffuser extends to a transitional curved section which, in turn, extends to a horizontal outlet section offset from the horizontal inlet section to shield observation of infrared and microwave signals from a downstream jet engine. A vane between the inlet and transitional curved sections further shields the observable signals and deflects inlet airflow against the interior wall of the diffuser for minimizing separation of boundary layer airflow from the wall. A backward facing slot is formed in the wall transversely adjacent the vane for effecting low energy boundary airflow to further minimize boundary layer airflow separation.

Abstract: The insulation panel (26) includes a corrugated sheet (28) having a fibrous blanket of insulation (32) secured thereto and an end cap (41) secured to an upper portion of the corrugated sheet (28). The end cap (41) provides a means by which an upper portion of the panel (26) may be anchored to a vertical structural wall (11) to be insulated and a means by which a panel (26) in a next upper row may be supported. After installation, fastening means (43) between the end cap (41) and the corrugated sheet (28) is removed to allow the upper portion of the corrugated sheet (28) to float in the end cap (41) and compensate for thermal expansion and contraction. In another embodiment of the panel (26a), the fastening means (43a) between the end cap (41) and the corrugated sheet (28) is frangible and shears in two upon expansion and contraction of the corrugated sheet (28).