J. A. Laurmann

• Development of a transonic slotted working section in the NAE 30-inch x 16-inch wind tunnel
• Slip flow over a short flat plate
• Stability of the compressible laminar boundary layer with an external pressure gradient
• The momentum integral method applied to the compressible boundary layer with a slip boundary condition
• Use of a double expansion method for solution of the incompressible viscous flow over a flat plate
• Use of a free molecule probe in high speed rarefied gas flow studies