Jeffrey E. Haas · 12 obras en el catálogoObrasCCold-air performance of a 12.766-centimeter-tip aixial-flow Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbineCCold-air performance of a 12.766-centimeter-tip-diameter axiCold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbineCCold-air performance of a 12.766-centimeter-tip aixial-flow Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbineEEffect of coolant flow ejection on aerodynamic performance oEffect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanesRReasons for low aerodynamic performance of 13.5-centimeter-tReasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbineAAnalytical and experimental investigation of stator endwall Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbineAAnalytical and experimental investigation of stator endwall Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbineRReactivation study for NASA Lewis Research Center's HypersonReactivation study for NASA Lewis Research Center's Hypersonic Tunnel FacilityCCold-air performance of a 12.766-centimeter-tip-diameter axiCold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbineEEffect of coolant flow ejection on aerodynamic performance oEffect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanesNNew hypersonic facility capability at NASA Lewis Research CeNew hypersonic facility capability at NASA Lewis Research CenterCCold-air performance of a 12.766-centimeter-tip axial-flow cCold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine
CCold-air performance of a 12.766-centimeter-tip aixial-flow Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine
CCold-air performance of a 12.766-centimeter-tip-diameter axiCold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine
CCold-air performance of a 12.766-centimeter-tip aixial-flow Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine
EEffect of coolant flow ejection on aerodynamic performance oEffect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes
RReasons for low aerodynamic performance of 13.5-centimeter-tReasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine
AAnalytical and experimental investigation of stator endwall Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
AAnalytical and experimental investigation of stator endwall Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine
RReactivation study for NASA Lewis Research Center's HypersonReactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility
CCold-air performance of a 12.766-centimeter-tip-diameter axiCold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine
EEffect of coolant flow ejection on aerodynamic performance oEffect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes
NNew hypersonic facility capability at NASA Lewis Research CeNew hypersonic facility capability at NASA Lewis Research Center
CCold-air performance of a 12.766-centimeter-tip axial-flow cCold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine