Publications
87 results found
Leishman B A, 2007, Mechanism of the Interaction of a Ramped Bleed Slot with the Primary Flow, ASME Journal of Turbomachinery, Vol: 129
Leishman B A, Cumpsty N A, Denton J D, 2007, Effects of Inlet Ramp Surfaces on the Aerodynamic Behaviour of Bleed Hole and Bleed Slot Off-Take Configurations, ASME Journal of Turbomachinery, Vol: 129
Cumpsty NA, Horlock JH, 2006, Averaging nonuniform flow for a purpose, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 128, Pages: 120-129, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 112
Gbadebo SA, Cumpsty NA, Hynes TP, 2005, Three-dimensional separations in axial compressors, International Gas Turbine and Aeroengine Congress and Exhibition, Publisher: ASME-AMER SOC MECHANICAL ENG, Pages: 331-339, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 239
Gbadebo SA, Hynes TP, Cumpsty NA, 2004, Influence of surface roughness on three-dimensional separation in axial compressors, 49th International Gas Turbine and Aeroengine Congress and Exhibition, Publisher: ASME, Pages: 455-463, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 79
Cumpsty NA, Greitzer EM, 2004, Ideas and methods of turbomachinery aerodynamics: A historical view, JOURNAL OF PROPULSION AND POWER, Vol: 20, Pages: 15-26, ISSN: 0748-4658
- Author Web Link
- Cite
- Citations: 28
Cumpsty NA, 2004, Compressor Aerodynamics, Publisher: 1989 Longman Scientific and Technical, 2004 Krieger, ISBN: 9781575242477
Leishman B A, Cumpsty N A, 2003, Arrangements for guiding bleed air in a gas turbine engine, GB2388875
Cumpsty NA, 2003, Jet Propulsion, Cambridge, Publisher: Cambridge University Press, ISBN: 9780521541442
Gallimore SJ, Bolger JJ, Cumpsty NA, et al., 2002, The use of sweep and dihedral in multistage axial flow compressor blading - Part I: University research and methods development, 47th International Gas Turbine and Aeroengine Congress and Exhibition, Publisher: ASME, Pages: 521-532, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 129
Gallimore SJ, Bolger JJ, Cumpsty NA, et al., 2002, The use of sweep and dihedral in multistage axial flow compressor blading - Part II: Low and high-speed designs and test verification, International Gas Turbine and Aeroengine Congress and Exhibition, Publisher: ASME-AMER SOC MECHANICAL ENG, Pages: 533-541, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 74
Cumpsty NA, 2001, Discussion: "Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex" ( Mailach, R., Lehmann, I., and Vogeler, K., 2001, ASME J. Turbomach., 123, no. 3, pp. 453-460), JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 123, Pages: 461-461, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 5
Cumpsty NA, 2001, Discussion: "Direct method for optimization of a centrifugal compressor vaneless diffuser" ( Lee, Y.-T., Luo, L., and Bein, T. W., 2001, ASME J. Turbomach., 123, pp, 73-79), JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 123, Pages: 79-80, ISSN: 0889-504X
Cumpsty NA, 2001, Discussion: "Comparative studies on short and long length-scale stall cell propagating in an axial compressor rotor" ( Inoue, M., Kuroumaru, M., Tanino, T., Yoshida, S., and Furukawa, M,, 2001, ASME J. Turbomach., 123, pp. 24-30), JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 123, Pages: 31-31, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 2
Shum YKP, Tan CS, Cumpsty NA, 2000, Impeller-diffuser interaction in a centrifugal compressor, 45th International Gas Turbine and Aeroengine Congress and Exhibition, Publisher: ASME, Pages: 777-786, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 82
Cumpsty NA, 2000, Discussion: "The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade" [ASME J. Turbomach., 122, No. 3, pp. 416-424 (2000)], JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 424-424, ISSN: 0889-504X
Cumpsty NA, 2000, Discussion: "Development of advanced compressor airfoils for heavy-duty gas turbines - Part II: Experimental and theoretical analysis" [ASME J. Turbomach., 122, No. 3, pp. 406-414 (2000)], JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 414-415, ISSN: 0889-504X
Cumpsty NA, 2000, Discussion: "On the development and application of the fast-response aerodynamic probe system in turbomachines - Part 3: Comparison of averaging methods applied to centrifugal compressor measurements" - [ASME J. Turbomach., 122, No. 3, pp. 527-535 (2000)], JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 536-536, ISSN: 0889-504X
Cumpsty NA, Freeman C, 2000, Comment on "Shock-loss model for transonic and supersonic axial compressors with curved blades", JOURNAL OF PROPULSION AND POWER, Vol: 16, Pages: 166-167, ISSN: 0748-4658
- Author Web Link
- Cite
- Citations: 1
Deniz S, Greitzer EM, Cumpsty NA, 2000, Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers: Part 2 - Straight channel diffuser - Authors' closure, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 19-21, ISSN: 0889-504X
Deniz S, Greitzer EM, Cumpsty NA, 2000, Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers: Part 2 - Straight channel diffuser, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 11-17, ISSN: 0889-504X
- Author Web Link
- Cite
- Citations: 36
Cumpsty NA, 2000, Propagation of multiple short-length-scale stall cells in an axial compressor rotor - Discussion, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 53-53, ISSN: 0889-504X
Cumpsty NA, 2000, Experimental and numerical investigation of the flow in a centrifugal compressor volute - Discussion, JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, Vol: 122, Pages: 30-30, ISSN: 0889-504X
Shun YPK, Tan CS, Cumpsty NA, 2000, Impeller-Diffuser interaction in centrifugal compressor, Transactions of the ASME, Journal of Turbomachinery, Vol: 122, Pages: 777-787
Deniz S, Greitzer EM, Cumpsty NA, 2000, Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers Part II: Straight-Channel Diffusers, Transactions of the ASME, Journal of Turbomachinery, Vol: 122
Train L, Cumpsty NA, 2000, Compressor blade leading edges in subsonic compressible flow, Journal of Mechanical Engineering Science, Proc Institution of Mechanical Engineers Part C, Pages: 221-242
Fillipenco VG, Greitzer EM, Deniz S, et al., 2000, Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers Part I: discrete-passage diffusers, Transactions of the ASME, Journal of Turbomachinery, Vol: 122, Pages: 1-10
Cumpsty NA, Freeman C, 1999, Supersonic blade performance, AIAA Journal of Propulsion and Power, Vol: 15
Khalid SA, Khalsa AS, Waitz IA, et al., 1999, Endwall blockage in axial compressors, Transactions of the ASME, Journal of Turbomachinery, Vol: 121, Pages: 499-509
Cumpsty, NA lead author, 1999, Aircraft Technology and its Relation to Emissions:Aviation and the Global Atmosphere, a special report of the Intergovenermental Panel on Climate Change, Aviation and the Global Atmospher, Editors: al, ISBN: 9780521664042
This data is extracted from the Web of Science and reproduced under a licence from Thomson Reuters. You may not copy or re-distribute this data in whole or in part without the written consent of the Science business of Thomson Reuters.