Tamara A. Smith

• Boundary layer development as a function of chamber pressure in the NASA Lewis 1030:1 area ratio rocket nozzle
• Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
• Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia)