Results 321 to 330 of about 24,787 (347)
Some of the next articles are maybe not open access.
Stall inception phenomena in a single-stage axial-flow pump
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2003The paper describes an experimental investigation on stall inception phenomena in a single-stage axial-flow pump, utilizing an oil flow technique and two different photo techniques. Moreover, the unsteady casing wall pressure was measured. Representative results are shown and discussed: the pump characteristic for two different NPSH values, selected ...
I Goltz +4 more
openaire +1 more source
Mid-Span Stall Inception in Low-Pressure-Ratio Transonic Fans
Journal of TurbomachineryAbstract In this paper, steady and unsteady computational fluid dynamics (CFD) have been used to investigate stall inception for a modern low-pressure-ratio transonic fan. The computational results are validated against measurement data from a high-speed test facility. CFD validation was approached as a blind test case.
H. Verschueren, C. A. Hall, M. J. Wilson
openaire +1 more source
Correlation and Prediction of Rotating Stall Inception by Divergence Method
Journal of Fluids Engineering, 1985An empirical correlation of rotating stall inception points of elementary compressors (isolated rotors, stages without prerotation, complete single stages, and multi-stage machines with repeating stages), modeled as equivalent diffusers, is presented. From it, two inception criteria for self-induced rotating stall are derived. Compressor blade rows are
openaire +1 more source
Integrative oncology: Addressing the global challenges of cancer prevention and treatment
Ca-A Cancer Journal for Clinicians, 2022Jun J Mao,, Msce +2 more
exaly
Axial Compressor Rotor Flow Structure at Stall-Inception
44th AIAA Aerospace Sciences Meeting and Exhibit, 2006Roger Davis, Jixian Yao
openaire +1 more source
Characterization of Stall Inception in High-Speed Single-Stage Compressors.
1994Abstract : Two single-stage, transonic compressor designs were tested under various undistorted operating conditions to characterize the process leading up to aerodynamic stall. The rig case was instrumented with eight high-response static pressure transducers equally spaced around the annulus for stall development detection. High-response measurements
openaire +1 more source
Multidisciplinary standards of care and recent progress in pancreatic ductal adenocarcinoma
Ca-A Cancer Journal for Clinicians, 2020Aaron J Grossberg +2 more
exaly
Oral complications of cancer and cancer therapy
Ca-A Cancer Journal for Clinicians, 2012Joel B Epstein +2 more
exaly

