Journal of Engineering and Sustainable Development, 2015 Experimental and numerical investigations to study the effect number of blade on the rotating stall phenomenon and pressure fluctuations in centrifugal blower.
Muna Sabah Kassim +2 more
doaj
Fluid machines: Expanding the limits, past and future [PDF]
During the 40 yr period from 1940 to 1980, the capabilities and operating limits of fluid machines were greatly extended. This was due to a research program, carried out to meet the needs of aerospace programs. Some of the events are reviewed.
Hartmann, M. J., Sandercock, D. M.
core +1 more source
Test techniques for obtaining off-nominal compressor data during engine tests [PDF]
Several unique techniques and related devices are described which are in use at the Lewis Research Center for off-design testing of fan and compressor sections in full-scale jet engines.
Biesiadny, T. J.
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Instrumentation Strategies for Monitoring Flow in Centrifugal Compressor Diffusers: Techniques and Case Studies. [PDF]
Sensors (Basel)Prisăcariu EG, Dumitrescu O.
europepmc +1 more source
Numerical Study on Local Entropy Production Mechanism of a Contra-Rotating Fan. [PDF]
Entropy (Basel), 2023 Jia X, Zhang X.
europepmc +1 more source
Comparison of two- and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor [PDF]
Two and three dimensional inviscid solutions for the flow in a transonic axial compressor rotor at design speed are compared with probe and laser anemometers measurements at near-stall and maximum-flow operating points.
Chima, R. V., Strazisar, A. J.
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Study of casing treatment stall margin improvement phenomena [PDF]
The results of a program of experimental and analytical research in casing treatments over axial compressor rotor blade tips are presented. Circumferential groove, axial-skewed slot, and blade angle slot treatments were tested.
Hilvers, D. E. +2 more
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Nonlinear Analysis of Rotating Stall
Journal of the Japan Society for Aeronautical and Space Sciences, 1970 openaire +2 more sources
Enhancing start-up and torque in Darrieus VAWTs through a novel plain gurney flap design. [PDF]
Sci RepEltayeb W +4 more
europepmc +1 more source
The performance evaluation of a jet flap on an advanced supersonic harrier [PDF]
The performance concept of a supersonic vertical and short takeoff and landing (V/STOL) fighter, model 279-3, modified to utilize a jet flap was evaluated.
Lipera, L. D., Sandlin, D. R.
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