PulseExploreJournal ClubDebatesTrendingResearchersJournals
Instagram
HomeExploreJournal ClubTrending
Synapse
⌘+K
Synapse
January 1, 1974The Aeronautical Journal168 citations

The effects of end plates on the base pressure coefficient of a circular cylinder

View Full Paper
PSPeter Stansby

Key Points

Key points are not available for this paper at this time.

Abstract

It has been known for some time that when a cylinder spans a wind tunnel the boundary layers on the walls of the tunnel may have important effects, especially on the pressure in the base region. By making the boundary layers thin by the use of end plates, it may be possible to approach a complete elimination of the effects of these layers on the central part of the span and obtain a flow that is very nearly two-dimensional. Most of the published pressure distributions for circular cylinders were obtained without end plates and this probably explains their inconsistency. Gerrard has described experiments in which the addition of end plates caused a substantial change of base pressure coefficient but he did not attempt to design an optimum end plate to give nearly two-dimensional flow.

Ask AI
Helpful
Bookmark
Share
View Full Paper

Cite This Study

Peter Stansby (1974) studied this question.

synapsesocial.com/papers/6a11e536f7bd4f5c7da582bfhttps://doi.org/10.1017/s0001924000036319
Ask AI
Helpful
Bookmark
Share
View Full Paper

Also Consider

Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context:

  1. 1A disturbance-sensitive Reynolds number range of the flow past a circular cylinder1965 · 115 citations
  2. 2The transition to turbulence in the wake of a circular cylinder1964 · 665 citations
  3. 3An experimental investigation of the oscillating lift and drag of a circular cylinder shedding turbulent vortices1961 · 128 citations
  4. 4The Dust Problem in Hot-Wire Anemometry1954 · 18 citations
  5. 5On the drag and shedding frequency of two-dimensional bluff bodies1954 · 679 citations