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Over the past 30 years, leading experts in turbomachinery unsteady aerodynamics, aer- coustics, and aeroelasticity from around the world have gathered to present and discuss recent advanc… Meer...

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[EAN: 9789048170913], Neubuch, [SC: 2.4], [PU: Springer Netherlands], ACC; DIN; INTELLIGENTSPEEDADAPTION; ROTOR; TURBINE; ADAPTIVECRUISECONTROL; CONTROL; DEVELOPMENT; MANAGEMENT; MODEL; S… Meer...

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ISBN: 9789048170913

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Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - pocketboek

2010, ISBN: 9048170915

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Bijzonderheden over het boek
Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines

This textbook is a collection of technical papers that were presented at the 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines held September 8-11, 2003 at Duke University in Durham, North Carolina. The papers represent the latest in state of the art research in the areas of aeroacoustics, aerothermodynamics, computational methods, experimental testing related to flow instabilities, flutter, forced response, multistage, and rotor-stator effects for turbomachinery.

Gedetalleerde informatie over het boek. - Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines


EAN (ISBN-13): 9789048170913
ISBN (ISBN-10): 9048170915
Gebonden uitgave
pocket book
Verschijningsjaar: 2010
Uitgever: Hall, Kenneth C. Kielb, Robert E. Thomas, Jeffrey P. Springer
640 Bladzijden
Gewicht: 1,004 kg
Taal: eng/Englisch

Boek bevindt zich in het datenbestand sinds 2011-09-16T00:19:09+02:00 (Amsterdam)
Detailpagina laatst gewijzigd op 2022-03-17T17:49:50+01:00 (Amsterdam)
ISBN/EAN: 9789048170913

ISBN - alternatieve schrijfwijzen:
90-481-7091-5, 978-90-481-7091-3


Gegevens van de uitgever

Auteur: Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas
Titel: Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines
Uitgeverij: Springer; Springer Netherland
626 Bladzijden
Verschijningsjaar: 2010-11-10
Dordrecht; NL
Gedrukt / Gemaakt in
Gewicht: 1,006 kg
Taal: Engels
249,98 € (DE)
256,99 € (AT)
275,50 CHF (CH)
POD
XII, 626 p.

BC; Previously published in hardcover; Hardcover, Softcover / Technik/Maschinenbau, Fertigungstechnik; Maschinenbau; Verstehen; ACC; DIN; Intelligent Speed Adaption; Rotor; Turbine; adaptive cruise control; control; development; management; model; simulation; thermodynamics; turbomachinery; vibration; C; Mechanical Engineering; Automotive Engineering; Engineering, general; Machinery and Machine Elements; Mechanical Engineering; Automotive Engineering; Technology and Engineering; Machinery and Machine Elements; Engineering; Fahrzeugbau; Ingenieurswesen, Maschinenbau allgemein; Maschinenbau; BB

Foreword. Preface. Part 1: Flutter-Flutter boundaries for pairs of low pressure turbine blades-Influence of a vibration amplitude-A method to assess flutter stability of complex modes-Flutter design of low pressure turbine blades with cyclic symmetric modes-Experimental and numerical investigation of 2D palisade flutter for the harmonic oscillations-Possibility of active cascade flutter control with smart structure in transonic flow condition-Experimental flutter investigations of an annular compressor cascade: influence of reduced frequency on stability.- Part 2: Forced responses-Unsteady gust response in the frequency domain-Axial turbine blade vibrations induced by the stator flow-Mistuning and coupling effects in turbomachinery bladings-Evalution of the principle of aerodynamic superposition in forced response calculations-Comparison of models to predict low engine order excitation in a high pressure turbine stage-Experimental reduction of transonic fan forced response by IGV flow control.- Part 3: Multistage effects-Unsteady aerodynamic work on oscillating annular cascades in counter rotation-Stucture of unsteady vortical wakes behind blades of mutual-moving rows of an axial turbomachine-The effect of mach number on LP turbine wake-blade interaction-Multistage coupling for unsteady flows in turbomachinery- Part 4: Aeroacoustics- Passive noise control by vane lean and sweep-Interaction of acoustic and vortical disturbances with an annular cascade in a swirling flow-Influence of mutual circumferential shift of stators on the noice generated by systems of rows stator-rotor-stator of the axial compressor-A frequency-domain solver for the non-linear propagation and radiation of fan noise- Part 5: Flow instabilities-Analysis of unsteady casing-Core compressor rotating stall simulation with a multi-bladerow model-Parametric study of surface roughness and wake unsteadiness on a flat plate with large pressure gradient-Bypass flow pattern changes at turbo-ram transient operation of combined cycle engine-Experimental investigation of wake-induced transition in a highly loaded linear compressor cascade-Experimental off-design investigation of unsteady secondary flow phenomena in a three-stage axial compressor at 100% nomial speed-Analyses of URANS and LES- Part 6: Computational techniques-Frequency and time domain-Study of shock movement and unsteady pressure on 2D generic model-Numerical unsteady aerodynamics for turbomachinery aeroelasticity-Development of an efficient and robust linearised navier-stokes flow solver-Optimized dual-time stepping technique for time-accurate navier-stokes calculations- Part 7: Experimental unsteady aerodynamics-Experimental and numerical study of nonlinear interactions in two-dimensional transonic nozzle flow-Interaction between shock waves and cascaded blades-Measured and calculated unsteady pressure field in a vaneless diffuser of a centrifugal compressor-DPIV measurements of the flow field between a transonic rotor and an upstream stator-Unsteady pressure management with correction on tubing distortion- Part 8: Aerothermodynamics-Unsteady 3D navier-stokes-Analysis of unsteady aerothermodynamic effects in a turbine-combustor- Part 9: Rotor stator interaction-Stator-rotor aeroelastic interaction for the turbine last stage in 3D transonic flow-Effects of stator clocking in systems of rows-Rotor-stator interaction in a highly loaded, single-stage, unsteady measurments in the rotor relative frame-Two-stage turbine experimental investigations of unsteady stator-to-stator interaction.

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