Titlebook: Drag Reduction by Shock and Boundary Layer Control; Results of the Proje Egon Stanewsky,Jean Délery,Paolo Matteis Conference proceedings 20

Covenant

書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control影響因子(影響力)




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control影響因子(影響力)學(xué)科排名




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control網(wǎng)絡(luò)公開(kāi)度




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control被引頻次




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control被引頻次學(xué)科排名




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control年度引用




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control年度引用學(xué)科排名




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control讀者反饋




書(shū)目名稱(chēng)Drag Reduction by Shock and Boundary Layer Control讀者反饋學(xué)科排名

SOW

Vassiliki Avgerinou,Stefanos G. Giakoumatosol on buffet onset..Two airfoils have been considered for the computations: the laminar DRA-2303 and the turbulent RAE-5225. Both airfoils were tested at DERA and hence experimental results were available allowing to make comparisons between the predicted numerical results and those obtained experimentally.

infelicitous

Vassiliki Avgerinou,Stefanos G. Giakoumatosr damping of buffet. The 3D-unsteady code VIS25, developed at ONERA as an extension of the 2D VIS 15 code, has finally been used to study sweep effects on the flow with and without bump in the case of the ADIF sheared wing.

Cabinet

災(zāi)難

Hybrid and Active Control of Shock Wave — Turbulent Boundary Layer Interaction and Perforated Plate tension of the transpiration law has been derived which takes into account the effect of tangential stream along a porous plate..Numerical simulations have been extended to a 3-D analysis of the flow in a channel Here, it was found that 3-D effects are responsible for the discrepancy between experiment and 2-D calculations performed earlier.

nettle

nettle

討好美人

An Investigation of Active, Suction, Shock and Boundary Layer Control Techniquesfiguration of Active Suction does not reduce drag, but theoretical parametric studies have revealed a potential control system, which could be examined by a simple modification to the existing system. Hybrid Suction is shown to be in-effective at reducing drag.

同步信息

Introduction to the Individual Contributions of the work performed by the various members of EUROSHOCK II, written by these members. The contributions, Chapters 11 through 24, are assembled in the order of the four tasks which comprise the research project. The sequence of the individual contributions and the main contents of the research performed are briefly outlined below.

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