Jeffrey E. Haas

• Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
• Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
• Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine
• Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine
• Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
• Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine
• Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine
• Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes
• Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes
• New hypersonic facility capability at NASA Lewis Research Center
• Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility
• Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine