A theoretical analysis of the fluid mechanics of the air cushion of th
e air reversers used in web-handling systems is presented. A two-dimen
sional model of the airflow is derived by averaging the equations of c
onservation of mass and momentum over the clearance between the web an
d the reverser. The resulting equations are Euler's equations with non
linear source terms representing the air supply holes in the surface o
f the reverser. The equations are solved analytically for the one-dime
nsional case and numerically for the two-dimensional case. Results are
compared with an empirical formula and the one-dimensional air-jet th
eory developed for hovercraft. Conditions that maximize the air pressu
re supporting the web are analyzed and design guidelines are deduced.