New hypersonic facility capability at NASA Lewis Research CenterJeffrey E. Haas · First published 1989Open the Tome
Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel FacilityJeffrey E. Haas · First published 1987Open the Tome
Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbineJeffrey E. Haas · First published 1982 · Latest edition 1984Open the Tome
Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbineJeffrey E. Haas · First published 1981Open the Tome
Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbineJeffrey E. Haas · First published 1977Open the Tome
Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbineJeffrey E. Haas · First published 1977Open the Tome
Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbineJeffrey E. Haas · First published 1977Open the Tome
Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanesJeffrey E. Haas · First published 1977Open the Tome
