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Jeffrey E. Haas

All books by Jeffrey E. Haas

(Displaying 12 Books)

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

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

Jeffrey E. Haas

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

Jeffrey E. Haas

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

Jeffrey E. Haas

Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine

Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine

Jeffrey E. Haas

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

Jeffrey E. Haas

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

Jeffrey E. Haas

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

Jeffrey E. Haas

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

Jeffrey E. Haas

New hypersonic facility capability at NASA Lewis Research Center

New hypersonic facility capability at NASA Lewis Research Center

Jeffrey E. Haas

Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility

Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility

Jeffrey E. Haas

Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine

Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine

Jeffrey E. Haas

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