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標(biāo)題: Titlebook: New Results in Numerical and Experimental Fluid Mechanics II; Contributions to the Wolfgang Nitsche,Hans-Joachim Heinemann,Reinhard H Book [打印本頁(yè)]

作者: DEIFY    時(shí)間: 2025-3-21 16:09
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作者: Noctambulant    時(shí)間: 2025-3-21 22:50
Wolfgang Nitsche,Hans-Joachim Heinemann,Reinhard HState of the Art der Str?mungsmechanik in Europa
作者: AWE    時(shí)間: 2025-3-22 03:27

作者: VEN    時(shí)間: 2025-3-22 06:05

作者: 碎石頭    時(shí)間: 2025-3-22 11:07

作者: 鎮(zhèn)痛劑    時(shí)間: 2025-3-22 13:56

作者: Texture    時(shí)間: 2025-3-22 18:08
New Results in Numerical and Experimental Fluid Mechanics IIContributions to the
作者: 檢查    時(shí)間: 2025-3-23 01:04
sis—This section considers payback periods, present worth analysis, return on investment, internal rate of return, benefit/cost ratios and positive-negative project balances; risk techniques of sensitivity analysis, optimistic-pessimistic analysis, discrete probability examples, and continuous proba
作者: BRAND    時(shí)間: 2025-3-23 03:15

作者: Indent    時(shí)間: 2025-3-23 09:35

作者: 犬儒主義者    時(shí)間: 2025-3-23 11:44
M. Baumann,D. Sturzebecher,W. Nitschesis—This section considers payback periods, present worth analysis, return on investment, internal rate of return, benefit/cost ratios and positive-negative project balances; risk techniques of sensitivity analysis, optimistic-pessimistic analysis, discrete probability examples, and continuous proba
作者: 下級(jí)    時(shí)間: 2025-3-23 17:00
S. Becker,F. Durst,H. Lienhartsis—This section considers payback periods, present worth analysis, return on investment, internal rate of return, benefit/cost ratios and positive-negative project balances; risk techniques of sensitivity analysis, optimistic-pessimistic analysis, discrete probability examples, and continuous proba
作者: SIT    時(shí)間: 2025-3-23 21:32
J. Birkemeyersis—This section considers payback periods, present worth analysis, return on investment, internal rate of return, benefit/cost ratios and positive-negative project balances; risk techniques of sensitivity analysis, optimistic-pessimistic analysis, discrete probability examples, and continuous proba
作者: 過(guò)渡時(shí)期    時(shí)間: 2025-3-23 23:47

作者: Offset    時(shí)間: 2025-3-24 03:25

作者: GRE    時(shí)間: 2025-3-24 08:44

作者: Gratuitous    時(shí)間: 2025-3-24 13:25
Guido Dietz,Stefan M?hlmann,Stefan Heinate” ends and means of achieving security in Israeli terms. Indeed, the strategic culture framework could provide a useful tool for anticipating how the Jewish state might come to grips with its ongoing internal, as well as external, security challenges.
作者: 傳染    時(shí)間: 2025-3-24 16:08
E. Elsholz,H. Steinmeyer,D. Johnate” ends and means of achieving security in Israeli terms. Indeed, the strategic culture framework could provide a useful tool for anticipating how the Jewish state might come to grips with its ongoing internal, as well as external, security challenges.
作者: 昏迷狀態(tài)    時(shí)間: 2025-3-24 19:00

作者: 紅腫    時(shí)間: 2025-3-25 03:00

作者: 同音    時(shí)間: 2025-3-25 06:47
A. Fezer,M. Klokerinutility of the nearly ninety years of scholarship that have been devoted to that highly scholarunfriendly subject, the causes of war. Just about everything that has been written on the subject with a view to developing a general theory of the causes of war has been a thorough waste of effort. The
作者: analogous    時(shí)間: 2025-3-25 10:22

作者: 谷物    時(shí)間: 2025-3-25 13:16
O. Brodersen,E. Monsen,A. Ronzheimer,R. Rudnik,C.-C. Rossow
作者: 防止    時(shí)間: 2025-3-25 16:26

作者: 愛(ài)得痛了    時(shí)間: 2025-3-25 22:58
On Active Control of Boundary Layer Instabilities on a Wing,ling-wave is successfully used for attenuation of natural occurring TS-waves on a wing. The actuator is driven by a digital signal processor, executing an adaptive filter algorithm to perform feedforward control of the wave cancellation process. A high attenuation of TS-waves is obtained not only in
作者: dowagers-hump    時(shí)間: 2025-3-26 03:52
Computation of Aerodynamic Coefficients for the DLR-F6 Configuration using MEGAFLOW,ion to the Baldwin-Lomax model, first computations using the . turbulence model from Wilcox are presented. The pressure distributions as well as the lift and drag coefficients are compared to wind tunnel measurements for both configurations. The comparison shows a good quality of the numerical resul
作者: 眼界    時(shí)間: 2025-3-26 06:18

作者: Encoding    時(shí)間: 2025-3-26 12:23
H. Bieler,R. Aleweltositive-negative project balances; risk techniques of sensitivity analysis, optimistic-pessimistic analysis, discrete probability examples, and continuous proba978-3-031-79393-6978-3-031-79394-3Series ISSN 2690-0300 Series E-ISSN 2690-0327
作者: AGONY    時(shí)間: 2025-3-26 14:41

作者: 食料    時(shí)間: 2025-3-26 20:15
Impact of Stringer-Width on the Effect of Hybrid Laminar Flow with Suction,with increased stringer width, suction chamber failure and outflow from a suction chamber..It comes out that within limits concessions to the ease of manufacturing or to other systems for a commercial application might be balanced with higher suction rates and therefore higher power requirements for the HLF system.
作者: Sinus-Node    時(shí)間: 2025-3-26 20:59

作者: Prophylaxis    時(shí)間: 2025-3-27 04:26

作者: 聯(lián)合    時(shí)間: 2025-3-27 07:31
Entropy-Layer Instabilities in Plane Supersonic Flow, wall-normal distribution of the mass-flow eigenfunction of the most amplified entropy-layer instability is found in hot-wire data. The streamwise wave number and the wall-normal phase distribution of the numerically obtained density eigenfunctions agree with a Schlieren picture.
作者: exquisite    時(shí)間: 2025-3-27 12:57
Book 1999programm der Bundesregierung (German Aeronautical Research Programme). Some of the papers report on work sponsored by the Deutsche Forschungsgemeinschaft, DFG, which also was presented at the symposium. The volume gives a broad overview over the ongoing work in this field in Germany.
作者: 廢止    時(shí)間: 2025-3-27 13:58

作者: 粗鄙的人    時(shí)間: 2025-3-27 19:23

作者: CRP743    時(shí)間: 2025-3-28 01:49
Pressure Sensitive Paint Application in Low-Speed Flows,Xenon — flash lamp and a nitrogen-laser were used for paint excitation and the resulting fluorescence fields in two spectral band length were acquired by 16 bit CCD slow scan camera with appropriate filters. Results shows that the optical pressure measurement system with binary paint can achieve pressure resolution better than 1 mbar.
作者: GNAT    時(shí)間: 2025-3-28 04:47

作者: 糾纏,纏繞    時(shí)間: 2025-3-28 07:42
0179-9614 ynamics Association). In this association those scientists and engineers from universities, research-establishments and industry are involved, who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics for aerospace and other applications. Many of the cont
作者: Diskectomy    時(shí)間: 2025-3-28 12:47
Effect of mean Flow Accuracy on PSE Results,ow data with sufficient precision are needed..We consider here the effect of systematic streamwise changes of the outer boundary condition on the PSE results for a well defined model flow (2D wedge flow). It is shown that boundary layer and stability computations react very sensitive to small changes in the outer boundary condition.
作者: hematuria    時(shí)間: 2025-3-28 16:23

作者: CURB    時(shí)間: 2025-3-28 19:13

作者: 彎曲的人    時(shí)間: 2025-3-29 01:41

作者: CON    時(shí)間: 2025-3-29 04:21

作者: Ophthalmoscope    時(shí)間: 2025-3-29 10:47

作者: 鐵塔等    時(shí)間: 2025-3-29 13:06
In-flight Boundary Layer Investigations on a Laminar Wing using Laser Doppler Anemometry,presented. In order to characterise the development of the Tollmien-Schlichting wave spectral and harmonic analysis were adopted. Finally, suggestions for further advancements of the LDA systems are proposed.
作者: 傻    時(shí)間: 2025-3-29 17:34
Strake Effects On the Turbulent Fin Flowfield Of a High-Performance Fighter Aircraft,r for the strake-on compared to the strake-off configuration. Moreover, the observed narrow-band concentration of turbulent kinetic energy is also less severe that the excitation level on fin structural modes is reduced.
作者: 制定    時(shí)間: 2025-3-29 23:18

作者: Gustatory    時(shí)間: 2025-3-30 00:37

作者: PAN    時(shí)間: 2025-3-30 07:10

作者: 舊病復(fù)發(fā)    時(shí)間: 2025-3-30 08:58
Control of flow separation by dynamic excitation of the free shear layer,d blowing through a narrow slot close to the leading edge of the airfoil. A small cavity below the slot was connected to a horn-driver providing periodic pressure fluctuations to drive the flow through the slot. The present research confirms the results of previous studies [1] that the mechanism for
作者: 圓桶    時(shí)間: 2025-3-30 14:05
On Active Control of Boundary Layer Instabilities on a Wing,in a reduction of the viscous friction drag. One less known approach is the reduction of natural occurring instability waves, so called Tollmien-Schlichting-waves (TS-waves) of a laminar boundary layer by means of superposition with artificially excited canceling waves. For technical applications of
作者: 宇宙你    時(shí)間: 2025-3-30 17:43

作者: 我不明白    時(shí)間: 2025-3-30 21:31

作者: MODE    時(shí)間: 2025-3-31 03:22

作者: 寄生蟲(chóng)    時(shí)間: 2025-3-31 05:51

作者: Hemiparesis    時(shí)間: 2025-3-31 09:43





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