Robert E. Kielb
Affiliations: | Mechanical Engineering and Materials Science | Duke University, Durham, NC |
Area:
Mechanical Engineering, Aerospace EngineeringGoogle:
"Robert Kielb"Children
Sign in to add traineeTomokazu Miyakozawa | grad student | 2008 | Duke |
Meredith A. Spiker | grad student | 2008 | Duke |
Fanny M. Besem | grad student | 2015 | Duke |
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Publications
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Hegde S, Mao Z, Pan T, et al. (2019) Separation of Up and Downstream Forced Response Excitations of an Embedded Compressor Rotor Journal of Turbomachinery-Transactions of the Asme. 141 |
Gutierrez M, Petrie-Repar P, Kielb RE, et al. (2018) A Mistuned Forced Response Analysis of an Embedded Compressor Blisk Using a Reduced Order Model Journal of Engineering For Gas Turbines and Power-Transactions of the Asme. 141: 32505 |
Li J, Aye-Addo N, Kielb R, et al. (2018) Mistuned Higher-Order Mode Forced Response of An Embedded Compressor Rotor, Part II: Mistuned Forced Response Prediction Journal of Turbomachinery-Transactions of the Asme. 140: 31006 |
Besem FM, Kielb RE. (2017) Influence of the Tip Clearance on a Compressor Blade Aerodynamic Damping Journal of Propulsion and Power. 33: 227-233 |
Besem FM, Kielb RE, Galpin P, et al. (2016) Mistuned forced response predictions of an embedded rotor in a multistage compressor Journal of Turbomachinery. 138 |
Waite JJ, Kielb RE. (2016) The impact of blade loading and unsteady pressure bifurcations on low-pressure turbine flutter boundaries Journal of Turbomachinery. 138 |
Besem FM, Kamrass JD, Thomas JP, et al. (2016) Vortex-Induced Vibration and Frequency Lock-In of an Airfoil at High Angles of Attack Journal of Fluids Engineering, Transactions of the Asme. 138 |
Besem FM, Thomas JP, Kielb RE, et al. (2016) An aeroelastic model for vortex-induced vibrating cylinders subject to frequency lock-in Journal of Fluids and Structures. 61: 42-59 |
Li J, Kielb RE. (2015) Effects of blade count ratio on aerodynamic forcing and mode excitability Proceedings of the Asme Turbo Expo. 7 |
Meinzer CE, Bittner SL, Schmitt S, et al. (2015) Design of a single stage turbine for the quantification of aerodynamic damping Proceedings of the Asme Turbo Expo. 7 |