Download (9Mb) - tuprints
Download (9Mb) - tuprints
Download (9Mb) - tuprints
Erfolgreiche ePaper selbst erstellen
Machen Sie aus Ihren PDF Publikationen ein blätterbares Flipbook mit unserer einzigartigen Google optimierten e-Paper Software.
[67] G. Endicott, T. Sonoda, M. Olhofer, and T. Arima. Aerodynamic improvement of a transonic<br />
fan outlet guide vane using 3d design optimization. Proceedings of ASME Turbo Expo,<br />
(Paper number GT-2011-46363), 2011.<br />
[68] T. Sonoda, T. Arima, G. Endicott, and M. Olhofer. A new aerodynamic design concept for<br />
transonic swept fan outlet guide vanes. Proceedings of International Symposium on Air<br />
Breathing Engines, (Paper number 2011-1224), 2011.<br />
[69] G. Kröger, C. Cornelius, and E. Nicke. Rotor casing contouring in high pressure stages of<br />
heavy duty gas turbine compressors with large tip clearance heights. Proceedings of ASME<br />
Turbo Expo, (Paper number GT-2009-59626), 2009.<br />
[70] G. Kröger, C. Voss, E. Nicke, and C. Cornelius. Theory and application of axisymmetric<br />
endwall contouring for compressors. Proceedings of ASME Turbo Expo, (Paper number<br />
GT-2011-45624), 2011.<br />
[71] G. Kröger. Beeinflussung von Rotorspaltströmungen durch rotationssymmetrische Gehäusekonturen.<br />
PhD thesis, DLR, 2010.<br />
[72] C. Dorfner, E. Nicke, and C. Voss. Axis-asymmetric profiled endwall design using multiobjective<br />
optimization linked with 3d rans-flow simulations. Proceedings of ASME Turbo<br />
Expo, (Paper number GT-2007-27268), 2007.<br />
[73] C. Dorfner, A. Hergt, E. Nicke, and R. Mönig. Advanced non-axisymmetric endwall contouring<br />
for axial compressors by generating an aerodynamic separator - part 1: Principal<br />
cascade design and compressor application. ASME Journal of Turbomachinery, 133(Paper<br />
number 021026), April 2011. Issue 2.<br />
[74] A. Hergt, C. Dorfner, W. Steinert, E. Nicke, and H.-A. Schreiber. Advanced nonaxisymmetric<br />
endwall contouring for axial compressors by generating an aerodynamic<br />
separator - part 2: Experimental and numerical cascade investigation. ASME Journal of<br />
Turbomachinery, 133(Paper number 021027), April 2011. Issue 2.<br />
[75] A. Hergt, J. Klinner, W. Steinert, C. Dorfner, and E. Nicke. Detailed flow analysis of a<br />
compressor cascade with non-axisymmetric endwall contour. Proceedings of European<br />
Turbomachinery Conference, (Paper number 095), 2011.<br />
[76] N. Harvey. Some effects of non-axisymmetric end wall profiling on axial flow compressor<br />
aerodynamics. part 1: Linear cascade investigation. Proceedings of ASME Turbo Expo,<br />
(Paper number GT-2008-50990), 2008.<br />
[77] J. Lu, W. Chu, and Y. Wu. Effects of endwall profiling on axial flow compressor stage.<br />
Proceedings of ASME Turbo Expo, (Paper number GT-2009-59418), 2009.<br />
[78] S. Hu, X. Lu, H. Zhang, J. Zhu, and Q. Xu. Numerical investigation of a high-subsonic<br />
axial-flow compressor rotor with non-axisymmetric hub endwall. Journal of Thermal<br />
Science, 19(DOI: 10.1007/s11630-010-0014-8), April 2010. Issue 1.<br />
[79] V. Iliopoulou, I. Lepot, and P. Geuzaine. Design optimization of a hp compressor blade<br />
and its hub endwall. Proceedings of ASME Turbo Expo, (Paper number GT-2008-50293),<br />
2008.<br />
Literaturverzeichnis 103
Change language