Information for "A Review on Surface Modification of Airfoils Using Dimples"

Jump to: navigation, search

Basic information

Display titleA Review on Surface Modification of Airfoils Using Dimples
Default sort keyA Review on Surface Modification of Airfoils Using Dimples
Page length (in bytes)2
Page ID34813
Page content languageen - English
Page content modelwikitext
Indexing by robotsAllowed
Number of redirects to this page0

Page protection

EditAllow all users (infinite)
MoveAllow all users (infinite)

Edit history

Page creatorRM (talk | contribs)
Date of page creation12:50, 13 May 2017
Latest editorRubiat Mustak (talk | contribs)
Date of latest edit13:21, 6 January 2018
Total number of edits7
Total number of distinct authors4
Recent number of edits (within past 90 days)0
Recent number of distinct authors0
Retrieved from "https://www.openresearch.org/wiki/A_Review_on_Surface_Modification_of_Airfoils_Using_Dimples"
Facts about "A Review on Surface Modification of Airfoils Using Dimples"
RDF feed
Access API{{{API}}} +
Has Challenges{{{Challenges}}} +
Has DataCatalouge{{{Catalogue}}} +
Has Description{{{Description}}} +
Has Dimensions{{{Dimensions}}} +
Has DocumentationURLhttp://{{{DocumentationURL}}} +
Has Downloadpagehttp://{{{Download-page}}} +
Has EvaluationMethod{{{EvaluationMethod}}} +
Has ExperimentSetup{{{ExperimentSetup}}} +
Has GUI{{{GUI}}} +
Has Hypothesis{{{Hypothesis}}} +
Has InfoRepresentation{{{InfoRepresentation}}} +
Has Limitations{{{Limitations}}} +
Has NegativeAspects{{{NegativeAspects}}} +
Has PositiveAspects{{{PositiveAspects}}} +
Has Requirements{{{Requirements}}} +
Has Results{{{Results}}} +
Has Version{{{Version}}} +
Has abstractAn airfoil is a cross section of airplanes …
An airfoil is a cross section of airplanes wings. Wings of airplanes produce lift by creating pressure difference between upper and lower surface of wings. This so called lift enables the airplanes to fly helps them remain high in the sky. One of the major problems that an airplane experienced is flow separation .Which causes the reduction of lift and increment of drag. Drag is the resisting force of air. A lot of researchers working hard since few decades to minimize this flow separation effect. As a result of their hard working concept of vortex generator have been developed .Which delays the boundary layer separation. Though there are various types of vortex generators. In the present review a special type of vortex generator namely dimple is focused. Since last half of decades investigations related to dimples grew the attention of many researchers .A lot of numerical and experimental investigations have been conducted by several researchers around the world related to dimples effect on airplanes wings cross section or airfoils. The outcomes of those investigations are extremely tremendous. Those outcomes indicate that dimples of different size and shape can play a vital role in designing of airplanes wings. This present study or review try to sum up all of those researches in a nut shell.
up all of those researches in a nut shell. +
Has authorsRubiat Mustak +
Has conclusion{{{Conclusion}}} +
Has future work{{{Future work}}} +
Has motivation{{{Motivation}}} +
Has platform{{{Platform}}} +
Has vendor{{{vendor}}} +
Proposes Algorithm{{{ProposesAlgorithm}}} +
TitleA Review on Surface Modification of Airfoils Using Dimples +
Uses Framework{{{Framework}}} +
Uses Methodology{{{Methodology}}} +
Uses Toolbox{{{Toolbox}}} +