Understanding Unsteady Flow Features in Transonic Compressors

descriptionPublicationkeyboard_double_arrow_right Article 01 Nov 2007Publisher:Institute of Electrical and Electronics Engineers (IEEE)Journal:Computing in Science & Engineering, volume 9, pages 12-17 (issn: 1521-9615,

Copyright policy )

Authors: Steven E. Gorrell; Allan van de Wall; Fu-Lin Tsung;

doi: 10.1109/mcse.2007.130

Understanding Unsteady Flow Features in Transonic Compressors

- Summary
- Metrics

Abstract

Applying computational science and engineering to the design and analysis of high-performance compressors makes it possible to understand unsteady flow effects in gas turbine engines. Simulations have produced numerical data of greatly improved geometric, physical, and numerical fidelity than previously possible, helping next-generation engines achieve unprecedented performance.

Related Organizations

GE Transportation
United States
United States Air Force Research Laboratory
United States
Wright-Patterson Air Force Base
United States

Impact byBIP!

	selected citations These citations are derived from selected sources. This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	1
	popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.	Average
	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Average
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average