Results 141 to 150 of about 4,884 (235)

Axial and Centrifugal Compressor Mean Line Flow Analysis Method [PDF]

open access: yes
This paper describes a method to estimate key aerodynamic parameters of single and multistage axial and centrifugal compressors. This mean-line compressor code COMDES provides the capability of sizing single and multistage compressors quickly during the ...
Veres, Joseph P.
core   +1 more source

Model equation for simulating flows in multistage turbomachinery [PDF]

open access: yes
A steady, three-dimensional average-passage equation system is derived for use in simulating multistage turbomachinery flows. These equations describe a steady, viscous flow that is periodic from blade passage to blade passage.
Adamczyk, J. J.
core   +1 more source

Influence of Regeneration-Induced Mistuning on the Aeroelasticity of Multistage Axial Compressors

open access: yes
AbstractCurrent developments in turbomachinery favor blade designs which are characterized by low damping. The associated reduction of structural damping, however, creates new problems such as higher vibration amplitudes. Therefore, accurate predictions of these vibration amplitudes and of the fatigue life become increasingly important.
Lukas Schwerdt   +4 more
openaire   +1 more source

Challenges, Opportunities and Future Directions of Membrane Technology for Natural Gas Purification: A Critical Review. [PDF]

open access: yesMembranes (Basel), 2022
Imtiaz A   +6 more
europepmc   +1 more source

Experimental Investigation of Rotating Stall in a Research Multistage Axial Compressor [PDF]

open access: yes
A collection of experimental data acquired in the NASA low-speed multistage axial compressor while operated in rotating stall is presented in this paper.
Braunscheidel, Edward P.   +2 more
core   +1 more source

High-speed neural imaging with multiplexed miniaturized two-photon microscopy. [PDF]

open access: yesCell Rep Methods
Zhang Z   +6 more
europepmc   +1 more source

Effect of steady-state temperature distortion and combined distortion on inlet flow to a turbofan engine [PDF]

open access: yes
Flow angle, static pressure, total temperature and total pressure were measured in the inlet duct upstream of a turbofan engine operating with temperature distortion or combined pressure-temperature distortion.
Bobula, G. A., Soeder, R. H.
core   +1 more source

Poster: Boundary Layer Separations in a Multistage Axial Compressor

open access: yes67th Annual Meeting of the APS Division of Fluid Dynamics - Gallery of Fluid Motion, 2014
Natalie R. Smith, Nicole L. Key
openaire   +1 more source

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