Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines

Front Cover
Kenneth C. Hall, Robert E. Kielb, Jeffrey P. Thomas
Springer Science & Business Media, Mar 8, 2006 - Technology & Engineering - 626 pages
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 advancements in the ?eld. The ?rst International Symposium on Unsteady Aero- namics, Aeroacoustics, and Aeroelasticity of Turbomachines (ISUAAAT) was held in Paris, France in 1976. Since then, the symposium has been held in Lausanne, Switzerland (1980), Cambridge, England (1984), Aachen, Germany (1987), Beijing, China (1989), Notre Dame, Indiana(1991), Fukuoka, Japan(1994), Stockholm, Sweden(1997), andLyon, France(2000). The Tenth ISUAAAT was held September 7-11, 2003 at Duke University in Durham, North Carolina. This volume contains an archival record of the papers presented at that meeting. The ISUAAAT, held roughly every three years, is the premier meeting of specialists in turbomachinery aeroelasticity and unsteady aerodynamics. The Tenth ISUAAAT, like its predecessors, provided a forum for the presentation of leading-edge work in turbomachinery aeromechanics and aeroacoustics of turbomachinery. Not surprisingly, with the continued development of both computer algorithms and computer hardware, the meeting featured a number of papers detailing computational methods for predicting unsteady ?ows and the resulting aerodynamics loads. In addition, a number of papers describing interesting and very useful experimental studies were presented. In all, 44 papers from the meeting are published in this volume.
 

Contents

Roque Corral Nelida Cerezal and Carlos Vasco
3
Olga V Chernysheva Torsten H Fransson Robert E Kielb and John Barter
17
Andrea Amone Francesco Poli and Claudia Schipani
31
Robert Kielb John Barter Olga Chemysheva and Torsten Fransson
41
Vladymir Tsimbalyuk Anatoly Zinkovskii Vitaly Gnesin Romuald Rzadkowski Jacek Sokolowski
53
Junichi Kazawa and Toshinori Watanabe
65
INFLUENCE OF REDUCED FREQUENCY ON STABILITY Joachim Belz and Holger Hennings
77
FORCED RESPONSE
93
X F Zhang H P Hodson
331
Shinichi Takata Toshio Nagashima Susumu Teramoto Hidekazu Kodama
345
Lothar Hilgenfeld and Michael Pfitzner
357
Andreas Bohne Reinhard Niehuis
369
P Ferrand J Boudet J Caro S Aubert C Rambeau
381
COMPUTATIONAL TECHNIQUES
395
DucMinh Tran and Cedric Liauzun
397
Davy AllegretBourdon Torsten H Fransson
409

A Filippone
95
Comparison of Calculations and Experiment M B Schmitz O Schafer J Szwedowicz T SecallWimmel TP Sommer
107
Gerhard Kahl
119
Stefan Schmitt Dirk Nurnberger Volker Carstens
133
Markus Jocker Alexandras Kessar Torsten H Fransson Gerhard Kahl HansJiirgen Rehder
145
S Todd Bailie Wing F Ng William W Copenhaver
161
MULTISTAGE EFFECTS
175
Combination of Supersonic and Subsonic Cascades M Namba K Nanba
177
VE Saren SA Smirnov
189
M Vera H P Hodson R Vazquez
203
Kenneth C Hall Kivanc Ekici and Dmytro M Voytovych
217
AEROACOUSTICS
231
B Elhadidi
233
H M Atassi A A Ali O V Atassi
247
D V Kovalev V E Saren and R A Shipov
261
Cyrille Breard
275
FLOW INSTABILITIES
291
S J Anderson CEng Dr N H S Smith CEng
293
M Vahdati A I Sayma M Imregun G Simpson
313
AnneSophie RougeaultSens and Alain Dugeai
423
Paul PetrieRepar
437
Mikhail Nyukhtikov Natalia V Smelova Brian E Mitchell D Graham Holmes
449
EXPERIMENTAL UNSTEADY AERODYNAMICS
461
Olivier Bron Pascal Ferrand and Torsten H Fransson
463
Shojiro Kaji Takahiro Suzuki Toshinori Watanabe
483
Teemu TurunenSaaresti Lappeenranta University of Technology Laboratory of Fluid Dynamics TeemuTurunenlutfi Jaakko Larjola
493
Steven E Gorrell William W Copenhaver Jordi Estevadeordal
505
H Yang D B SimsWilliams and L He
521
AEROTHERMODYNAMICS
531
Th Hildebrandt J Ettrich M Kluge M Swoboda A Keskin F Haselbach HP Schiffer
533
Horia C Flitan and Paul G A Cizmas Thomas Lippert and Dennis Bachovchin Dave Little
551
ROTOR STATOR INTERACTION
567
Romuald Rzadkowski Vitaly Gnesin Luba Kolodyazhnaya
569
I
581
II
603
III
615
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