CİLTLER LİSTELER GÜNLÜK AKTİVİTE İNCELEMELER Üyeler

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jeffrey e haas

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TurbinesCold-air performance of a 12.766-centimeter-tip axial-flow cooled turbineJeffrey E. Haas

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

Jeffrey E. Haas · for sale by the National Information Service

Sayfa sayısı yok · 1977

Gas-turbines / Rotors / Turbines

Turborjet enginesCold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbineJeffrey E. Haas

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

Jeffrey E. Haas · National Aeronautics and Space Administration, Scientific and Technical Information Office

35 sayfa · 1977

Aerodynamics / Cooling / Airplanes / Turborjet engines

Turborjet enginesEffect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanesJeffrey E. Haas

Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes

Jeffrey E. Haas · National Aeronautics and Space Administration, Scientific and Technical Information Office

31 sayfa · 1977

Aerodynamics / Cooling / Airplanes / Turborjet engines

High-speed aeronauticsNew hypersonic facility capability at NASA Lewis Research CenterJeffrey E. Haas

New hypersonic facility capability at NASA Lewis Research Center

Jeffrey E. Haas · For sale by the National Technical Informatio Service

Sayfa sayısı yok · 1989

High-speed aeronautics

TurbinesCold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbineJeffrey E. Haas

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

Jeffrey E. Haas · National Aeronautics and Space Administration, Scientific and Technical Information Office

Sayfa sayısı yok · 1977

Gas-turbines / Rotors / Turbines

Turbine-propeller enginesAnalytical and experimental investigation of stator endwall contouring in a small axial-flow turbineJeffrey E. Haas

Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine

Jeffrey E. Haas · National Aeronautics and Space Administration, Scientific and Technical Information Branch

20 sayfa · 1984

Airplanes / Aerodynamics / Turbines / Turbine-propeller engines

Hypersonic wind tunnelsReactivation study for NASA Lewis Research Center's Hypersonic Tunnel FacilityJeffrey E. Haas

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

Jeffrey E. Haas · For sale by the National Technical Information Service

Sayfa sayısı yok · 1987

Hypersonic wind tunnels

EvaluationReasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbineJeffrey E. Haas

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

Jeffrey E. Haas · National Aeronautics and Space Administration, Scientific and Technical Branch

16 sayfa · 1981

Airplanes / Motors / Evaluation