Zobrazeno 1 - 10
of 93
pro vyhledávání: '"Robert E. Kielb"'
Publikováno v:
Journal of Turbomachinery. 145
A lack of reliable experimental data on transonic blade flutter in real turbomachines hampers the further improvement of computational design predictions for off-design operation regimes of newly-built machines. Acquiring unsteady pressure distributi
Publikováno v:
Journal of Turbomachinery. 145
Boundary-layer ingestion systems have the potential to improve propulsion efficiency using fluid with lower momentum near the airframe. However, they also bring variations in the velocity and total pressure, leading to a complex distortion of the flo
Publikováno v:
Volume 2C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions.
This paper expands upon a multi-degree-of-freedom, Van der Pol oscillator used to model buffet and Nonsynchronous Vibrations (NSV) in turbines. Two degrees-of-freedom are used, a fluid tracking variable incorporating a Van der Pol oscillator and a cl
Publikováno v:
Volume 9A: Structures and Dynamics — Aerodynamics Excitation and Damping; Bearing and Seal Dynamics; Emerging Methods in Design and Engineering.
This paper focuses on the impact of hub labyrinth seal leakage flows on the aeromechanical behavior of an embedded compressor rotor. End wall flows are critical in determining the performance of gas turbine engine compressors, particularly the hub le
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
Shreyas Hegde, Robert E. Kielb
Publikováno v:
AIAA Scitech 2021 Forum.
Autor:
Robert E. Kielb, Fanny M. Besem
Publikováno v:
Journal of Propulsion and Power. 33:227-233
The flutter CFD calculations conducted in industry generally use a single-row, single-passage approach with a minimum of detailing to reduce the computational time as much as possible. The question arises of what level of detailing is necessary for a
Publikováno v:
Journal of Turbomachinery. 141
The aerodynamic interaction of upstream and downstream blade rows can have a significant impact on the forced response of the compressor. Previously, the authors carried out the forced response analysis of a three-row stator-rotor-stator (S1-R2-S2) c
Publikováno v:
AIAA Scitech 2019 Forum.
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 141
Accuracy when assessing mistuned forced response analyses is still a major concern. Since a fully coupled analysis is still very computational expensive, several simplifications and reduced-order models (ROMs) are carried out. The use of a reduction