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1.
Regular marked price:
$100.00
Discount Price:
$77.40
Cost Savings:
$22.60 (23%)
Price fluctuation possible.
Corporate Finance and Governance
Author name:
Lawrence E. Mitchell
,
Lawrence A. Cunningham
,
Jeffrey J. Haas
,
Lewis D. Solomon
January 30, 2006
2.
Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine (NASA technical paper)
Author name:
Jeffrey E Haas
1982
3.
Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine (NASA technical paper)
Author name:
Jeffrey E Haas
1977
4.
Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes: I--performance with coolant ejection holes plugged (NASA technical memorandum ; NASA TM X-3395)
Author name:
Jeffrey E Haas
1976
5.
Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes: II-performance with coolant flow ejection at temperature ratios up to 2 (NASA technical paper)
Author name:
Jeffrey E Haas
1977
6.
Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine (NASA technical paper)
Author name:
Jeffrey E Haas
1981
7.
Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility (SuDoc NAS 1.15:89918)
Author name:
Jeffrey E. Haas
1981
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