Three wing sections FX66‐S‐196VI, E603 and AH82–150A were analyzed. Measured data of these wing sections are published. First wing section was measured in Stuttgart University and in Delft University of Technology, when other two wing sections were measured in Stuttgart University. These wing sections have different behavior in the region of maximum lift. FX66‐S‐196VI wing section has sharp drop in lift. The stall of the second and third wing sections is smooth, though different. All wing sections are affected by laminar separation bubbles. The calculations were performed using three codes: Eppler Program System, XFOIL and RFOIL. Eppler's code uses non‐interacted inviscid plus boundary layer method. Influence of separation is estimated usin...
This collection of data on airfoils has been made from the published reports of a number of the lead...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2001Thesis (M.Sc.) -- ...
Wings on airplanes and Unmanned Aerial Vehicles (UAVs) have a very important role in the formation o...
Three wing sections FX66‐S‐196VI, E603 and AH82–150A were analyzed. Measured data of these wing sect...
The transition location on the FX 66-S-196 V1 wing section was analyzed with the using interactive p...
A comparison of predicted and measured laminar‐turbulent transition on the airfoil is presented. The...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
In this article history and development of calculation methods of wing characteristics are presented...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Airfoil plays an important role in any aircraft and chooses whether the lift power is adequate to ad...
This paper attempts to discover the structural behavior of the wing imperiled to flowing loads throu...
The object of this report is to bring together the investigations of the various aerodynamic laborat...
MEng (Mechanical Engineering), North-West University, Potchefstroom CampusXFOIL is a fast and relati...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This collection of data on airfoils has been made from the published reports of a number of the lead...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2001Thesis (M.Sc.) -- ...
Wings on airplanes and Unmanned Aerial Vehicles (UAVs) have a very important role in the formation o...
Three wing sections FX66‐S‐196VI, E603 and AH82–150A were analyzed. Measured data of these wing sect...
The transition location on the FX 66-S-196 V1 wing section was analyzed with the using interactive p...
A comparison of predicted and measured laminar‐turbulent transition on the airfoil is presented. The...
Calculation results for 11 different finite span wings are presented. Calculations were made by a co...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
In this article history and development of calculation methods of wing characteristics are presented...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Airfoil plays an important role in any aircraft and chooses whether the lift power is adequate to ad...
This paper attempts to discover the structural behavior of the wing imperiled to flowing loads throu...
The object of this report is to bring together the investigations of the various aerodynamic laborat...
MEng (Mechanical Engineering), North-West University, Potchefstroom CampusXFOIL is a fast and relati...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
This collection of data on airfoils has been made from the published reports of a number of the lead...
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 2001Thesis (M.Sc.) -- ...
Wings on airplanes and Unmanned Aerial Vehicles (UAVs) have a very important role in the formation o...