An air inlet section (40) for an aircraft propulsion system nacelle (24) includes an outer skin (48), an inner skin (50), and a lip skin (54). The lip skin (54) extends between and to an outer end (70) and an inner end (72). The outer end (70) is disposed ...

The invention concerns a heat transfer arrangement for a fluid-washed body (25;123;124) having first (26;128) and second (32;132) ends and a fluid-washed surface extending there-between. The arrangement comprises a heat transfer member (28;133) extending f...