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The steady laminar supersonic flow past a flat plate having a stretch of anelastic membrane, the pressure on the other side of which is adjustable, isstudied within the framework of the triple deck theory. The resulting lowerdeck problem is supplemented with a membrane equation relating the pressuredifference across the membrane to its curvature. By pressurizing ordepressurizing the membrane, it assumes the form of a hump or a dent thatalters the flow characteristics. Numerical solutions obtained, in either case,give plausible account of the interaction between the membrane and the flow.

Supersonic triple deck flow past a flat plate with an elastic stretch