Titlebook: Aircraft Wake Turbulence and Its Detection; Proceedings of a Sym John H. Olsen,Arnold Goldburg,Milton Rogers Conference proceedings 1971 Pl

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書目名稱Aircraft Wake Turbulence and Its Detection影響因子(影響力)




書目名稱Aircraft Wake Turbulence and Its Detection影響因子(影響力)學科排名




書目名稱Aircraft Wake Turbulence and Its Detection網絡公開度




書目名稱Aircraft Wake Turbulence and Its Detection網絡公開度學科排名




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書目名稱Aircraft Wake Turbulence and Its Detection被引頻次學科排名




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書目名稱Aircraft Wake Turbulence and Its Detection年度引用學科排名




書目名稱Aircraft Wake Turbulence and Its Detection讀者反饋




書目名稱Aircraft Wake Turbulence and Its Detection讀者反饋學科排名

Detoxification

Das Maschinenzeichnen des Konstrukteursollows one of two patterns, depending on whether Q is less than or greater than a critical value Qcrit. If Q < Qcrit, the circulation decreases more rapidly than the momentum and the vortices separate as they descend to an equilibrium level. If Q > Qcrit, the momentum of the vortices decreases more

Alpha-Cells

https://doi.org/10.1007/978-3-662-29212-9film element. For Reynolds numbers less than approximately 5 × 10., the heat flux to the upstream split film is greater than the downstream. This is used to detect the sense of the velocity component normal to the sensor. Such information from all three orthogonal sensors yields the octant of the ai

弄污

Anordnung der Ansichten und Schnitte,difficult to separate the various mechanisms responsible for the vortex decay..This paper describes a pilot study of trailing vortices using a sub-scale model in a more controllable laboratory environment. The essential feature of this laboratory facility is to have a vortex-generating wing moving a

火海

Das Maschinenzeichnen des Konstrukteursce structure. Limited flight tests with a dissipater fitted to a Convair 990 wing tip and using a Lear jet aircraft as a probe indicated that the rolling acceleration and the degree of roll control required was less in the modified vortex than in the unmodified vortex.

逢迎春日

Gesamtzeichnungen und sonstige Zeichnungen,d a 13-foot-span C-130 wind-tunnel model, mounted in a 23-foot by 16-foot working section, showed remarkable coherence until the adverse pressure gradient in the wind-tunnel diffuser caused vortex bursting. The effects, on vortex burst posi-tion in the diffuser, of auxiliary blowing into or near the

笨拙處理

,Abgekürzte, vereinfachte Darstellung,exhausts of certain aircraft with wing mounted engines..Vortex flow velocities were obtained using hot-film/hot-wire sensors..Measured tangential velocities were approximately double those velocities predicted by certain theory (which assumes an elliptical lift distribution) ..Distinct vortex charac

托人看管

,Der Konstrukteur und das Werkstück,are two distinct mechanisms advanced for vortex wake decay-- the slowing down of the vortices by mixing action of eddy viscosity, and the interaction of the vortices with each other, which disorganizes the organized vortex flow field. The slowing down by eddy viscosity is conceptually simple, but is

Saline

labile

Studies in the Motion and Decay of Vorticesviscid theory ignores the diffusion of vorticity in the core. For a general three dimensional problem, the present scheme of analysis can be carried out provided the shape of the vortex line and the three dimensional flow field fulfill a constraint condition. This condition is automatically fulfille