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Unsteady Aerodynamics, Aeroacoustics

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Unsteady Aerodynamics, Aeroacoustics
and Aeroelasticity of Turbomachines
Edited by
KENNETH C. HALL
ROBERT E. KIELB
JEFFREY P. THOMAS


Table of Contents 

Part I  Flutter

1  Flutter Boundaries for Pairs of Low Pressure Turbine Blades

2  Influence of a Vibration Amplitude Distribution on the Aerodynamic Stability of a Low-Pressure Turbine Sectored Vane

3  A Method to Assess Flutter Stability of Complex Modes

4  Flutter Design of Low Pressure Turbine Blades with Cyclic Symmetric Modes

5  Experimental and Numerical Investigation of 2D Palisade Flutter for the Harmonic Oscillations

6  Possibility of Active Cascade Flutter Control with Smart Structure in Transonic Flow Condition

7  Experimental Flutter Investigations of an Annular Compressor Cascade: Influence of Reduced Frequency on Stability

Part II Forced Response

8  Unsteady Gust Response in the Frequency Domain

9  Axial Turbine Blade Vibrations Induced by the Stator Flow

10 Mistuning and Coupling Effects in Turbomachinery Bladings

11 Evaluation of the Principle of Aerodynamic Superposition in Forced Response Calculations

12 Comparison of Models to Predict Low Engine Order Excitation in a High Pressure Turbine Stage

13 Experimental Reduction of Transonic Fan Forced Response by IGV Flow Control

Part III Multistage Effects

14 Unsteady Aerodynamic Work on Oscillating Annular Cascades in Counter Rotation

15 Structure of Unsteady Vortical Wakes behind Blades of Mutual-Moving Rows of an Axial Turbomachine

16 The Effect of Mach Number on LP Turbine Wake-Blade Interaction

17 Multistage Coupling for Unsteady Flows in Turbomachinery

Part IV Aeroacoustics

18 Passive Noise Control by Vane Lean and Sweep

19 Interaction of Acoustic and Vortical Disturbances with an Annular Cascade in a Swirling Flow

20 Influence of Mutual Circumferential Shift of Stators on the Noise Generated by System of Rows Stator-Rotor-Stator of the Axial Compressor

21 A Frequency-domain Solver for the Non-linear Propagation and Radiation of Fan Noise

Part V Flow Instabilities

22 Analysis of Unsteady Casing Pressure Measurements During Surge and Rotating Stall

23 Core-Compressor Rotating Stall Simulation with a Multi-Bladerow Model

24 Parametric Study of Surface Roughness and Wake Unsteadiness on a Flat Plate with Large Pressure Gradient

25 Bypass Flow Pattern Changes at Turbo-Ram Transient Operation of a Combined Cycle Engine

26 Experimental Investigation of Wake-Induced Transition in a Highly Loaded Linear Compressor Cascade

27 Experimental Off-Design Investigation of Unsteady Secondary Flow Phenomena in a Three-Stage Axial Compressor

28 Analyses of URANS and LES Capabilities to Predict Vortex Shedding for Rods and Turbines

Part VI Computational Techniques

29 Frequency and Time Domain Fluid-Structure Coupling Methods for Turbomachineries

30 Study of Shock Movement and Unsteady Pressure on 2D Generic Model

31 Numerical Unsteady Aerodynamics for Turbomachinery Aeroelasticity

32 Development of an Efficient and Robust Linearised

33 Optimized Dual-Time Stepping Technique for Time-Accurate Navier-Stokes Calculations

Part VII Experimental Unsteady Aerodynamics

34 Experimental and Numerical Study of Nonlinear Interactions in Two-Dimensional Transonic Nozzle Flow

35 Interaction Between Shock Waves and Cascaded Blades

36 Measured and Calculated Unsteady Pressure Field in a Vaneless Diffuser of a Centrifugal Compressor

37 DPIV Measurements of the Flow Field between a Transonic Rotor and an Upstream Stator

38 Unsteady Pressure Measurement with Correction on Tubing Distortion

Part VIII Aerothermodynamics

39 Unsteady 3D Navier-Stokes Calculation of a Film-Cooled Turbine Stage with Discrete Cooling Hole

40 Analysis of Unsteady Aerothermodynamic Effects in a Turbine-Combustor

Part IX Rotor Stator Interaction

41 Stator-Rotor Aeroelastic Interaction for the Turbine Last Stage in 3D Transonic Flow

42 Effects of Stator Clocking in System of Rows Stator-Rotor-Stator of the Subsonic Axial Compressor

43 Rotor-Stator Interaction in a Highly-Loaded, Single-Stage,Low-Speed Axial Compressor: Unsteady Measurements in the Rotor Relative Frame

44 Two-Stage Turbine Experimental Investigations of Unsteady Stator-to-Stator Interaction




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