標(biāo)題: Titlebook: Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines; Kenneth C. Hall,Robert E. Kielb,Jeffrey P. Thomas Conference pro [打印本頁] 作者: probiotic 時間: 2025-3-21 19:47
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines影響因子(影響力)
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines影響因子(影響力)學(xué)科排名
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines網(wǎng)絡(luò)公開度
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines被引頻次
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines被引頻次學(xué)科排名
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines年度引用
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines年度引用學(xué)科排名
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines讀者反饋
書目名稱Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines讀者反饋學(xué)科排名
作者: irreducible 時間: 2025-3-21 23:22
Robert Kielb,John Barter,Olga Chernysheva,Torsten Franssontrol and civil engineers working in sewage flow and wastewater treatment and of interest to academics wishing to see how their ideas on optimal control work out when practically applied..978-1-4471-5673-4978-1-84628-092-4Series ISSN 1430-9491 Series E-ISSN 2193-1577 作者: 責(zé)難 時間: 2025-3-22 02:53 作者: insincerity 時間: 2025-3-22 04:37
S. Todd Bailie,Wing F.Ng,William W. Copenhavere authors review well-established models and scheduling policies, under regular and irregular performance measures, respectively. Chapter 4 describes models with stochastic machine breakdowns. Chapters 5 and 6 978-1-4899-7884-4978-1-4899-7405-1Series ISSN 0884-8289 Series E-ISSN 2214-7934 作者: 狗窩 時間: 2025-3-22 12:09 作者: Anguish 時間: 2025-3-22 16:08 作者: BURSA 時間: 2025-3-22 20:40 作者: 性滿足 時間: 2025-3-22 21:13 作者: Mucosa 時間: 2025-3-23 02:42 作者: 鋼筆記下懲罰 時間: 2025-3-23 07:07
Junichi Kazawa,Toshinori Watanabe as multiple targets. The chapter starts, however, with the simpler situation of a single searcher looking for a single target. We formulate the optimal search problem as that of finding the optimal searcher path and describe a branch-and-bound algorithm for its solution. We proceed by generalizing 作者: 搜集 時間: 2025-3-23 12:23
Joachim Belz,Holger Henningse. The theory is applicable to those practical situations in which a dynamic system is sensitive to sampling or gives a different response at each run of the experiment. Together with the definition of group designs that is also introduced, this structure leads to a practical and numerically tractab作者: parsimony 時間: 2025-3-23 14:32 作者: libertine 時間: 2025-3-23 21:35 作者: 感情 時間: 2025-3-23 22:12 作者: NATTY 時間: 2025-3-24 02:26 作者: 蹣跚 時間: 2025-3-24 10:25
M. Vera,H.P. Hodson,R. Vazquezses fall even beyond this type of problems. A total of over 70 books has been devoted to structural optimization as yet, but none of them has treated stability constraints in a sufficiently broad and comprehensive manner. The purpose of the present book is to fill this gap. The contents include a di作者: 果核 時間: 2025-3-24 12:20 作者: macabre 時間: 2025-3-24 15:54 作者: Cervical-Spine 時間: 2025-3-24 20:43 作者: languor 時間: 2025-3-25 02:26
POSSIBILITY OF ACTIVE CASCADE FLUTTER CONTROL WITH SMART STRUCTURE IN TRANSONIC FLOWCONDITIONl the passage shock oscillation. The trailing edge oscillation might be realized by, for instance, application of piezo-electric device. The method was revealed to change the unsteady aerodynamic force acted on the blade from exciting to damping force if the phase of trailing edge oscillation was pr作者: Feedback 時間: 2025-3-25 03:28 作者: invulnerable 時間: 2025-3-25 07:45
EXPERIMENTAL REDUCTION OF TRANSONIC FAN FORCED RESPONSE BY IGV FLOW CONTROLnic resonance crossings. Sensitivity of resonant response amplitude to full-span TEB flowrate, as well as optimal TEB flowrates, are documented for multiple modes. Resonant response sensitivity was generally characterized by a robust region of substantial attenuation, such that less-than-optimal TEB作者: EPT 時間: 2025-3-25 14:57 作者: organism 時間: 2025-3-25 18:18
FLUTTER DESIGN OF LOWPRESSURE TURBINE BLADES WITH CYCLIC SYMMETRIC MODES very quick and easy to use. Theory and example applications are presented and compared with the results of full three-dimensional viscous CFD analyses. Reasonable agreement is found. The interaction effects of the cosine and sine modes and the work associated with the steady pressure are shown to generally be significant.作者: Flounder 時間: 2025-3-25 21:44
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF 2D PALISADE FLUTTER FOR THE HARMONIC OSCILLATIONSculations were carried out for the torsional and bending oscillations of the compressor cascade. The comparison of the calculated and experimental results for different conditions of the cascade oscillations has shown the good quantitative and qualitative agreement.作者: 無法解釋 時間: 2025-3-26 03:29
AXIAL TURBINE BLADE VIBRATIONS INDUCED BY THE STATOR FLOW transformed flow solution is transferred to the finite element model where the blade excitation is obtained. Two reduced geometrical rotor-stator configurations are investigated and compared with respect to the flow field and the resulting blade excitation.作者: catagen 時間: 2025-3-26 07:08
MISTUNING AND COUPLING EFFECTS IN TURBOMACHINERY BLADINGSy of the present method to accurately capture the dominant effects that influence the aeroelastic behavior of the cascades. Further case studies are performed to assess the influence of alternating and random mistuning on the resonant response amplitudes and on the aeroelastic stability.作者: 分發(fā) 時間: 2025-3-26 10:11
THE EFFECT OF MACH NUMBER ON LP TURBINEWAKE-BLADE INTERACTION reference to a profile designed using current low pressure turbine design practice. Wake traverses using pneumatic probes reveal that the unsteadiness reduced the profile losses up to Mach numbers of 0.9作者: 容易懂得 時間: 2025-3-26 15:32
Conference proceedings 2006f 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..作者: Painstaking 時間: 2025-3-26 20:33 作者: 租約 時間: 2025-3-26 22:51
areas of aeroacoustics, aerothermodynamics, computational methods, experimental testing related to flow instabilities, flutter, forced response, multistage, and rotor-stator effects for turbomachinery..978-90-481-7091-3978-1-4020-4605-6作者: FUSE 時間: 2025-3-27 04:22 作者: Spinal-Tap 時間: 2025-3-27 07:27 作者: OTTER 時間: 2025-3-27 10:16
FLUTTER DESIGN OF LOWPRESSURE TURBINE BLADES WITH CYCLIC SYMMETRIC MODES real mode shapes, baseline unsteady aerodynamic analyses must be performed for the 3 fundamental motions, two translations and a rotation. Unlike the current method work matrices must be saved for a range of reduced frequencies and interblade phase angles. These work matrices are used to generate t作者: Adulterate 時間: 2025-3-27 16:10
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF 2D PALISADE FLUTTER FOR THE HARMONIC OSCILLATIONSa for three-dimensional flows are currently hardly available in the published literature. Therefore comparisons between numerical methods and experimental ones for simple cascade geometry at inviscid flow conditions must play an essential role in validation of the three-dimensional unsteady solution作者: 拋棄的貨物 時間: 2025-3-27 18:30 作者: 廣大 時間: 2025-3-28 00:31
UNSTEADY GUST RESPONSE IN THE FREQUENCY DOMAIN of the admittance for side force and yawing moment under sinusoidal gust conditions. This approach provides indirectly the power spectra density (PSD), which is often used to characterize systems in unsteady periodic conditions (Filippone and Siquier, 2003, Filippone, 2003). The flow model is invis作者: VOK 時間: 2025-3-28 03:57 作者: BUOY 時間: 2025-3-28 08:13 作者: Injunction 時間: 2025-3-28 12:08
EVALUATION OF THE PRINCIPLE OF AERODYNAMIC SUPERPOSITION IN FORCED RESPONSE CALCULATIONSotating propfan features transonic flow conditions and aerodynamic interaction between the blade rows. The computed unsteady aerodynamics are verified by comparison with rig measurements. A forced response analysis based on the principle of superposition is conducted, similar to the current practice作者: CRAMP 時間: 2025-3-28 15:40 作者: BULLY 時間: 2025-3-28 19:58 作者: Etching 時間: 2025-3-29 02:48 作者: Radiculopathy 時間: 2025-3-29 06:53 作者: flammable 時間: 2025-3-29 07:42 作者: incisive 時間: 2025-3-29 11:29
Conference proceedings 2006and 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, flutt作者: 從容 時間: 2025-3-29 17:31
tion of technical papers that were presented at the 10.th. 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 作者: orient 時間: 2025-3-29 19:49
COMPARISON OF MODELS TO PREDICT LOW ENGINE ORDER EXCITATION IN A HIGH PRESSURE TURBINE STAGEumber and pressure are computed with poor agreement to experiments. Future evaluations of the resulting rotor excitation pressure are needed to estimate the level of necessary agreement to give acceptable predictions of the low engine order forced response.作者: majestic 時間: 2025-3-30 00:42
STRUCTURE OF UNSTEADY VORTICAL WAKES BEHIND BLADES OF MUTUAL-MOVING ROWS OF AN AXIAL TURBOMACHINEssing waves of vorticity causes acoustic disturbances and additional aerodynamical losses owing to energy dissipation. As dissipative function depends on distribution of vorticity, for an estimation of the losses, caused a rotor-stator interaction, the description of vortical wakes structure at presence in them of free vortexes is necessary.作者: 健談 時間: 2025-3-30 06:35
he conventional power generating plant will make a significant contribution to sustainable power production. Wind and solar energy resources are the promising sources of renewable energy. They have huge potential that can satisfy the energy demand and can reduce the emission of harmful greenhouse ga作者: 陪審團 時間: 2025-3-30 09:14 作者: 眼界 時間: 2025-3-30 13:53 作者: RAG 時間: 2025-3-30 19:30 作者: Osteoporosis 時間: 2025-3-30 21:55 作者: ALIEN 時間: 2025-3-31 02:31
Junichi Kazawa,Toshinori Watanabeers. The plan might call for an instantaneous shift of search effort from one time period to the next. If the searcher requires a significant amount of time to carry out this shift, a relatively fast moving target would “get ahead” of the searcher. This situation is especially prevalent in robotic s作者: 桉樹 時間: 2025-3-31 06:18 作者: 搖晃 時間: 2025-3-31 12:38
A. Filipponeook is an applications-oriented study of such physical systems; in particular, those which can be described by an elliptic partial differential equation and where the shape is found by the minimum of a single criterion function. There are many problems of this type in high-technology industries. In 作者: Exploit 時間: 2025-3-31 16:58
M. B. Schmitz,O. Sch?fer,J. Szwedowicz,T. Secall-Wimmel,T. P. Sommerithms and experiments.Contains practical applications in sec.This self-contained book describes social influence from a computational point of view, with a focus on recent and practical applications, models, algorithms and open topics for future research. Researchers, scholars, postgraduates and dev作者: 種子 時間: 2025-3-31 18:27
