標題: Titlebook: Numerical and Physical Aspects of Aerodynamic Flows IV; Tuncer Cebeci Conference proceedings 1990 Springer-Verlag Berlin Heidelberg 1990 a [打印本頁] 作者: 乳缽 時間: 2025-3-21 18:19
書目名稱Numerical and Physical Aspects of Aerodynamic Flows IV影響因子(影響力)
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書目名稱Numerical and Physical Aspects of Aerodynamic Flows IV讀者反饋學科排名
作者: 小說 時間: 2025-3-21 23:28 作者: 乳白光 時間: 2025-3-22 00:57 作者: 使習慣于 時間: 2025-3-22 05:13 作者: 緯線 時間: 2025-3-22 10:21
Hank E. Heliny international conferences following the Rio Earth Summit held in 1992. It has come to be clearly recognized among the scientific community that a great many of the climate disasters that occur frequently now are man-made, mainly through excessive emissions of greenhouse gases. It is also recognize作者: Myofibrils 時間: 2025-3-22 14:15 作者: Override 時間: 2025-3-22 18:10 作者: 完全 時間: 2025-3-22 21:25 作者: 去掉 時間: 2025-3-23 04:23
Stewartson Memorial Lecture: Experiments are Telling You Somethingpers dealing with experimental work. This is reflected in the programme for the Fourth Symposium of which this paper is a part. It is also apparent that considerably more attention is paid to calculations in the references cited, and this is understandable in view of national and international empha作者: 沒有希望 時間: 2025-3-23 08:14 作者: 小平面 時間: 2025-3-23 10:06
Coupling Procedures for Viscous-Inviscid Interaction for Attached and Separated Flows on Swept and Tns. At the high Reynolds numbers of aviation some part of the flow will be turbulent, and some form of turbulence model must be adopted along with the time-averaged form of the Navier-Stokes equations. Although there have been impressive advances in the numerical solution of these equations this app作者: 固定某物 時間: 2025-3-23 14:12
New Possibilities of Viscous-Inviscid Numerical Techniques for Solving Viscous Flow Equations with Marations. The progress removes however these restricting views, and the viscous-inviscid strategy appears more and more as a general computational technique for viscous flow equations in high Reynolds number aerodynamics.作者: 歸功于 時間: 2025-3-23 18:32 作者: Compatriot 時間: 2025-3-23 23:19 作者: 舊式步槍 時間: 2025-3-24 05:27 作者: 身體萌芽 時間: 2025-3-24 09:08 作者: aviator 時間: 2025-3-24 12:22
Calculation of Transonic Flows for Novel Engine-Airframe Installationsncorporates the superfan and the ultra-high-bypass (UHB) propulsion systems. The superfan engine is an advanced derivative of the turbofan powerplant, while the UHB concept employs a multibladed counterrotating unshrouded fan. A schematic top view of the airplane with the alternative engines is show作者: Canopy 時間: 2025-3-24 18:03 作者: Estrogen 時間: 2025-3-24 20:21
Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurationsto numerically approximate the solution of the QAZ1D form of the Euler equations presented in [208]. This formulation is unique in that the equations are written in terms of Riemann-type variables using a natural streamline coordinate system. Because of this, the equations model wave propagation in 作者: Excise 時間: 2025-3-24 23:33 作者: Isolate 時間: 2025-3-25 06:18
The Relevance of Unsteady Aerodynamics for Highly Maneuverable and Agile Aircraftics in the future. The combat arena will continue to be divided into the beyond-visualrange (BVR) and within-visual-range (WVR) areas of engagement, which will necessitate aircraft design trade-offs between stealth, performance, and maneuverability. The value of agile maneuverability is explicit in 作者: 小畫像 時間: 2025-3-25 09:09
Experimental and Computational Studies of Dynamic Stallited, rather than enhanced, helicopter flight. At the same time, retention of the dynamic lift that occurs when aircraft rapidly pitch past the static stall angle is critical if the full benefit of this lift augmentation for improved aircraft maneuverability is to be achieved. Thus, the alleviation 作者: perjury 時間: 2025-3-25 13:17 作者: 使絕緣 時間: 2025-3-25 19:43 作者: 最小 時間: 2025-3-25 20:27
Numerical Simulation of Separated and Vortical Flows on Bodies at Large Angles of Attackth and location of the leeward vortical flow and the location of the viscous layer separation lines has precluded accurate predictions of high-incidence flow with the more approximate techniques. Consequently, we have focused solely on Parabolized Navier-Stokes and time-marching Navier-Stokes comput作者: Blasphemy 時間: 2025-3-26 00:47 作者: Ingenuity 時間: 2025-3-26 07:14 作者: Motilin 時間: 2025-3-26 10:04 作者: overwrought 時間: 2025-3-26 13:29 作者: Arresting 時間: 2025-3-26 20:14
L. W. Carr,M. F. Platzer,M. S. Chandrasekhara,J. Ekaterinarisn from an international group of distinguished scholars whose impressive, forward-looking, and thought-provoking perspectives on relevant issues incite, broaden, and expand complicated conversations on how we m978-3-642-42835-7978-3-642-27702-3Series ISSN 1869-4918 Series E-ISSN 1869-4926 作者: 組裝 時間: 2025-3-27 00:13
Andrew M. Wo,Eugene E. Covertn from an international group of distinguished scholars whose impressive, forward-looking, and thought-provoking perspectives on relevant issues incite, broaden, and expand complicated conversations on how we m978-3-642-42835-7978-3-642-27702-3Series ISSN 1869-4918 Series E-ISSN 1869-4926 作者: 向外 時間: 2025-3-27 04:35
Lewis B. Schiff,David Degani,Russell M. Cummingsith the prospect only of grossly iniquitous progress being achieved and that too amidst environmental crises. If impending disasters are to be averted and genuine prosperity is to be seriously sought to benefit all, scientists and planners should have major parts to play.作者: 松果 時間: 2025-3-27 08:48 作者: N防腐劑 時間: 2025-3-27 09:49 作者: Enrage 時間: 2025-3-27 15:18 作者: Mirage 時間: 2025-3-27 17:56 作者: AMPLE 時間: 2025-3-28 00:03 作者: exigent 時間: 2025-3-28 05:26 作者: erythema 時間: 2025-3-28 06:46
Atlee M. Cunnigham Jr.r all.? .The research studies that are reported and discussed in the volume have been drawn from an international group of distinguished scholars whose impressive, forward-looking, and thought-provoking perspectives on relevant issues incite, broaden, and expand complicated conversations on how we m作者: Aspiration 時間: 2025-3-28 11:25
Predictions of Airfoil Aerodynamic Performance Degradation Due to IcingOne of the major elements of the NASA Aircraft Icing Research Program is the development and validation of a series of mutually compatible computer codes which predict the details of an aircraft icing encounter. These codes once validated can be used for:作者: evanescent 時間: 2025-3-28 16:41 作者: 考博 時間: 2025-3-28 21:03
New Possibilities of Viscous-Inviscid Numerical Techniques for Solving Viscous Flow Equations with Marations. The progress removes however these restricting views, and the viscous-inviscid strategy appears more and more as a general computational technique for viscous flow equations in high Reynolds number aerodynamics.作者: SLAY 時間: 2025-3-29 02:38 作者: 金哥占卜者 時間: 2025-3-29 04:35 作者: 隱語 時間: 2025-3-29 09:12
http://image.papertrans.cn/n/image/669258.jpg作者: 錯誤 時間: 2025-3-29 13:42 作者: 不開心 時間: 2025-3-29 18:12 作者: Nonthreatening 時間: 2025-3-29 22:28
Computational Fluid Dynamics at NASA Ames Research Centerss in the discipline at its current stage is incremental but still happening. Because of the demonstrated potential of CFD, the understood limitations of experimental and flight testing, and the rapid advances in computer hardware, the discipline of CFD has developed at an explosive pace.作者: Keratin 時間: 2025-3-30 02:32 作者: Commodious 時間: 2025-3-30 06:32
The Relevance of Unsteady Aerodynamics for Highly Maneuverable and Agile Aircraft time scales of unsteady flows which are driven by rapidly maneuvering aircraft, along with the influence of three dimensionality and localized compressibility, provide important insights into this complex problem.作者: 嘲弄 時間: 2025-3-30 10:47
VISTRAFS: A Simulation Method for Strongly Interacting Viscous Transonic Flowdue to increasing operational costs. Secondly, computational power is getting cheaper and numerical methods are improving, which makes it possible to perform more realistic flow simulations at reasonable cost. Another advantage of computational methods is their ability to be used in optimization studies.作者: 外星人 時間: 2025-3-30 15:21
Coupling Procedures for Viscous-Inviscid Interaction for Attached and Separated Flows on Swept and T time-averaged form of the Navier-Stokes equations. Although there have been impressive advances in the numerical solution of these equations this approach is still beyond the resources of the aircraft designer.作者: obtuse 時間: 2025-3-30 17:44 作者: inundate 時間: 2025-3-31 00:22 作者: arthroscopy 時間: 2025-3-31 03:02
A Critique of the Experimental Aerodynamic Data Base for an Oscillating Straked Wing at High Anglesome very important under such conditions. The understanding of these flow fields and dynamic effects is needed in order to design aircraft to exploit the concepts, however this represents several quantum jumps over current aerodynamic technology.作者: Measured 時間: 2025-3-31 05:18
Stewartson Memorial Lecture: Experiments are Telling You Somethingsis on less expensive research; but it does not mean that the physical aspects of laminar, transitional and turbulent flows are adequately understood. Nor does it mean that the lessons of experiments already performed should be neglected or ignored.作者: 是他笨 時間: 2025-3-31 11:02 作者: fulmination 時間: 2025-3-31 13:54
Calculation of Three-Dimensional Boundary Layers Including Hypersonic Flowss over cars or aircraft. As concerns space shuttles, the flow calculation must account for real gas effects. When nonequilibrium effects are important, resolution of the local boundary layer equations is needed.作者: 人造 時間: 2025-3-31 19:24
ch was held at the California State University, Long Beach, from 16-19 January 1989. It includes the Stewartson Memorial Lecture of Professor J. H. Whitelaw, and is divided into three parts. The first is a collection of papers that describe the status of current technology in two- and three-dimensio作者: 不可接觸 時間: 2025-4-1 01:26
10樓作者: anniversary 時間: 2025-4-1 03:39
10樓作者: 形容詞 時間: 2025-4-1 07:27
10樓作者: 頑固 時間: 2025-4-1 13:42
10樓
