Axial compressor aerodesign evolution at general electric

Journal of Turbomachinery

Volumn 124, Issue 3, 2002, Pages 321-330

  Smith Jr, Leroy H ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS;

SUBSONIC BLADING;

TURBOMACHINERY;

AXIAL COMPRESSOR; DESIGN; HISTORY;

EID: 0036648908     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1486219     Document Type: Article

References (23)

1. Early history of the axial type of gas turbine engine
2. Aerodynamic design and development of the general electric CJ805-23 aft fan component
3. The radial-equilibrium equation of turbomachinery
4. Some aerodynamic design consideration for high bypass ratio fans
5. Spanwise mixing in axial-flow turbomachines
6. Secondary flow, turbulent diffusion, and mixing in axial-flow compressors
7. Übet die Winkelübertreibung von Turbinenschaufeln
8. Discussion of "loss and stall analysis of compressor cascades"
9. Sweep and dihedral effects in axial-flow turbomachinery
10. Loss reduction in axial-flow compressors through low-speed model testing
11. Casing boundary layers in multistage axial-flow compressors
12. On the resistance to flow of water through pipes or passages having divergent boundaries
13. Recovery ratio - A measure of the loss recovery potential of compressor stages
14. Stalling pressure rise capability of axial flow compressor stages
15. Loss, sources and magnitudes in axial-flow compressors
16. NASA/GE fan and compressor research accomplishment