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ISBN: 9781402046056

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Unsteady Aerodynamics Aeroacoustics and Aeroelasticity of Turbomachines - nieuw boek

ISBN: 9781402046056

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Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas
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Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas:
Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - nieuw boek

2006

ISBN: 9781402046056

eBooks, eBook Download (PDF), 2006, [PU: Springer Netherlands], Seiten: 626, Springer Netherlands, 2006

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Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas
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Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas:
Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - nieuw boek

2006, ISBN: 9781402046056

eBooks, eBook Download (PDF), 2006, [PU: Springer Netherlands], Springer Netherlands, 2006

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Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas
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Kenneth C. Hall; Robert E. Kielb; Jeffrey P. Thomas:
Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines - eerste uitgave

2006, ISBN: 9781402046056

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


EAN (ISBN-13): 9781402046056
ISBN (ISBN-10): 1402046057
Verschijningsjaar: 2006
Uitgever: Springer Netherlands
626 Bladzijden
Taal: eng/Englisch

Boek bevindt zich in het datenbestand sinds 2007-01-22T02:43:24+01:00 (Amsterdam)
Detailpagina laatst gewijzigd op 2023-06-27T14:39:20+02:00 (Amsterdam)
ISBN/EAN: 1402046057

ISBN - alternatieve schrijfwijzen:
1-4020-4605-7, 978-1-4020-4605-6
alternatieve schrijfwijzen en verwante zoekwoorden:
Auteur van het boek: jeffrey thomas, kenneth thomas, robert thomas, thomas hall, robert ris, robert now
Titel van het boek: aeroelasticity, aerodynamics, aeroe aeroe, aeroelastic, turbomachines


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: 2006-05-11
Dordrecht; NL
Gedrukt / Gemaakt in
Taal: Engels
213,99 € (DE)
220,00 € (AT)
236,00 CHF (CH)
Available
XII, 626 p.

EA; E107; eBook; Nonbooks, PBS / 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; 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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