INTRODUCTION TO STEP WING & KLINE FOGLEMAN AIRFOIL |
Author(s): |
| prashant singh , MATS University; Prashant Singh, School Of engg.& IT.,MATS University; Sachin Ku. Shah, School Of engg.& IT.,MATS University; Saurabh Shriwas, School Of engg.& IT.,MATS University; kalpit p. kaurse, School Of engg.& IT.,MATS University |
Keywords: |
| Airfoil, Step wing, KF airfoil, Stall |
Abstract |
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This Paper is discussed with the study of the analysis of the concept of step wings with Kline-Fogleman airfoil. Here the study of analysis at different angle of attacks helps to conclude that the KF airfoil provides promising results against the stalling at higher angle of attack as well as in some configuration the lift generation is really appreciable. Here the entire KF and KFm family of airfoils are described along with their application. The concept of Kline Fogleman airfoil is associated with the step shaped geometry at the top and bottom surface of the airfoil. This airfoil was generated by the Richard Kline and Floyd Fogleman in 1960 for the paper planes. In this paper we will check the possibilities of its practical application. |
Other Details |
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Paper ID: IJSRDV3I2254 Published in: Volume : 3, Issue : 2 Publication Date: 01/05/2015 Page(s): 503-506 |
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