Hall K.C., Kielb R.E., Thomas J.P. (еds.) Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines

Springer, 2006. – 604 р. — ISBN-10 1-4020-4267-1; ISBN-13 978-1-4020-4267-6.Flutter.
Flutter Boundaries for Pairs of Low.
Pressure Turbine Blades.
Roque Corral, Nélida Cerezal, and Cárlos Vasco.
Influence of a Vibration Amplitude Distribution on the Aerodynamic.
Stability of a Low-Pressure Turbine Sectored Vane.
Olga V. Chernysheva, Torsten H. Fransson, Robert E. Kielb, and John Barter.
A Method to Assess Flutter Stability of Complex Modes.
Andrea Arnone, Francesco Poli, and Claudia Schipani.
Flutter Design of Low Pressure Symmetric Modes.
Robert Kielb, John Barter, Olga Chernysheva and Torsten Fransson.
Experimental and Numerical Investigation of 2D Palisade.
Flutter for the Harmonic Oscillations.
Vladymir Tsimbalyuk, Anatoly Zinkovskii, Vitaly Gnesin', Romuald Rzadkowski, Jacek Sokolowski.
Possibility of Active Cascade Flutter Control with Smart Structure in Transonic Flow Condition.
Turbine Blades with Cyclic.
Junichi Kazawa, and Toshinori Watanabe.
Experimental Flutter Investigations of an Annular Compressor Cascade.
Influence of Reduced Frequency on Stability.
Joachim Belz and Holger Hennings.
Forced Response/.
Unsteady Gust Response in the Frequency Domain.
A. Filippone.
Axial Turbine Blade Vibrations Induced by the Stator Flow.
M. B. Schmitz, O. Schäfer, J. Szwedowicz, T. Secall-Wimmel, T. P. Sommer.
Mistuning and Coupling Effects in Turbomachinery Bladings.
Gerhard Kahl.
Evaluation of the Principle of Aerodynamic Superposition in Forced Response Calculations.
Stefan Schmitt, Dirk Nürnberger, Volker Carstens.
Comparison of Models to Predict Low Engine Order Excitation in a High Pressure Turbine Stage.
Markus Jöcker, Alexandros Kessar, Torsten H. Fransson, Gerhard Kahl, Hans-Jürgen Rehder.
Experimental Reduction of Transonic Fan Forced Response by IGV Flow Control.
S. Todd Bailie, Wing F. Ng,William W. Copenhaver.
Multistage Effects.
Unsteady AerodynamicWork on Oscillating Annular Cascades in Counter Rotation.
M. Namba, K. Nanba.
Structure of Unsteady Vortical Wakes behind Blades of Mutual-Moving Rows of an Axial Turbomachine.
V.E.Saren, S.A. Smirnov.
The Effect of Mach Number on LP TurbineWake-Blade Interaction.
M. Vera, H. P. Hodson, R. Vazquez.
Multistage Coupling for Unsteady Flows in Turbomachinery.
Kenneth C. Hall, Kivanc Ekici and Dmytro M. Voytovych.
Aeroacoustics.
Passive Noise Control by Vane Lean and Sweep.
B. Elhadidi.
Interaction of Acoustic and Vortical Disturbances with an Annular Cascade in a Swirling Flow.
H. M. Atassi, A. A. Ali,, O. V. Atassi.
Influence of Mutual Circumferential Shift of Stators on the Noise Generated by System of Rows Stator-Rotor-Stator of the Axial Compressor.
D. V. Kovalev, V. E. Saren and R. A. Shipov.
A Frequency-domain Solver for the Non-linear Propagation and Radiation of Fan Noise.
Cyrille Breard.
Flow Instabilities.
Analysis of Unsteady Casing Pressure Measurements During Surge and Rotating Stall.
S. J. Anderson (CEng), Dr. N. H. S. Smith (CEng).
Core-Compressor Rotating Stall Simulation with a Multi-Bladerow Model.
M. Vahdati, A I Sayma, M Imregun, G. Simpson.
Parametric Study of Surface Roughness and Wake Unsteadiness on a Flat Plate with Large Pressure Gradient.
X. F. Zhang, H. P. Hodson.
Bypass Flow Pattern Changes at Turbo-Ram Transient Operation of a Combined Cycle Engine.
Shinichi Takata, Toshio Nagashima, Susumu Teramoto, Hidekazu Kodama.
Experimental Investigation of Wake-Induced Transition in a Highly Loaded Linear Compressor Cascade.
Lothar Hilgenfeld and Michael Pfitzner.
Experimental Off-Design Investigation of Unsteady Secondary Flow Phenomena in a Three-Stage Axial Compressor at 100% Nominal Speed.
Andreas Bohne, Reinhard Niehuis.
Analyses of URANS and LES Capabilities to Predict Vortex Shedding for Rods and Turbines.
P. Ferrand, J. Boudet, J. Caro, S. Aubert, C. Rambeau.
Computational Techniques.
Frequency and Time Domain Fluid-Structure Coupling Methods for Turbomachineries.
Duc-Minh Tran and Cédric Liauzun.
Study of Shock Movement and Unsteady Pressure on 2D Generic Model.
Davy Allegret-Bourdon, Torsten H. Fransson.
Numerical Unsteady Aerodynamics for Turbomachinery Aeroelasticity.
Anne-Sophie Rougeault-Sens and Alain Dugeai.
Development of an Efficient and Robust Linearised Navier-Stokes Flow Solver.
Paul Petrie-Repar.
Optimized Dual-Time Stepping Technique for Time-Accurate Navier-Stokes Calculations.
Mikhail Nyukhtikov, Natalia V. Smelova, Brian E. Mitchell, D. Graham Holmes.
Experimental Unsteady Aerodynamics.
Experimental and Numerical Study of Nonlinear Interactions.
Olivier Bron, Pascal Ferrand, and Torsten H. Fransson.
Interaction Between Shock Waves and Cascaded Blades.
Measured and Calculated Unsteady Pressure Field in a Vaneless Diffuser of a Centrifugal Compressor.
Teemu Turunen-Saaresti, Jaakko Larjola.
DPIV Measurements of the FlowField between a Transonic Rotor and an Upstream Stator.
Steven E. Gorrell, William W. Copenhaver, Jordi Estevadeordal.
Unsteady Pressure Measurement with Correction on Tubing Distortion.
H. Yang, D. B. Sims-Williams, and L. He.
Aerothermodynamics.
Unsteady 3D Navier-Stokes Calculation of a Film-Cooled Turbine Stage with Discrete Cooling Hole.
Th. Hildebrandt, J. Ettrich, M. Kluge, M. Swoboda, A. Keskin, F. Haselbach, H.-P. Schiffer.
Analysis of UnsteadyAerothermodynamic Effects in a Turbine-Combustor.
Horia C. Flitan and Paul G. A. Cizmas, Thomas Lippert and Dennis Bachovchin, Dave Little.
Part IX Rotor Stator Interaction.
Stator-Rotor Aeroelastic Interaction for the Turbine Last Stage in 3D Transonic Flow.
Romuald Rzadkowski, Vitaly Gnesin, Luba Kolodyazhnaya.
Effects of Stator Clocking in System of Rows Stator-Rotor-Stator of the Subsonic Axial Compressor.
N.M. Savin, V.E. Saren.
Rotor-Stator Interaction in a Highly-Loaded, Single-Stage, Low-Speed Axial Compressor: Unsteady Measurements in the Rotor Relative Frame.
O. Burkhardt,W. Nitsche, M. Goller, M. Swoboda, V. Guemmer, H. Rohkamm, and G.GoKosyna.
Two-Stage Turbine Experimental Investigations of Unsteady Stator-to-Stator Interaction.
Jan Krysinski, Robert Blaszczak Jaroslaw, Antoni Smolny.