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Experimental Study of the Wing Sweep Angle Effect on the Pressure Distribution of a Half Model
Agha Seyyed Jafari, Masoumeh | 2009
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- Type of Document: M.Sc. Thesis
- Language: Farsi
- Document No: 39207 (45)
- University: Sharif University of Technology
- Department: Aerospace Engineering
- Advisor(s): Soltani, Mohammad Reza
- Abstract:
- In this thesis the behavior of a 3D wing has investigated by Flow visualization and pressure acquisition test. The goal of this tests was considering changes in 3D wing section parameter in comparison with 2D airfoils. The performed Tests showed that variation in 3D wing treatment is affected by finite aspect ratio and sweep angle and also indicate changes in pressure profile, increasing pressure peak and decreasing effective speed. CFD studies has conducted to investigate special effect of sweep angle and show that lift and drag coefficient decrease with increasing sweep angle. Also different section pressure profile near the wing tip and intersection of wing/fuselage varies and miss optimum state
- Keywords:
- Three Dimentional Wing ; Pressure Profiles ; Sweep Angle ; Experimental Studies
- محتواي پايان نامه
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