Theoretical investigation of effects of channel walls on the pressure, lifts, and moment coefficients of a thin airfoil in a straight channel.

Date

1971

Author

Yeğen, Imdat

Metadata

Show full item record

Item Usage Stats

83
views

0
downloads

URI

https://hdl.handle.net/11511/6979

Collections

Graduate School of Natural and Applied Sciences, Thesis

Suggestions

OpenMETU
Core

Theoretical investigation of effects of suction and blowing on wall shear stress in the stagnation line region of a cylinder in a turbulent flow. Ilhan, Bahadır; Department of Mechanical Engineering (1970)
Theoretical investigation of the effects of the free stream oscillations on the boundary layer development and heat transfer in the vicinity of stagnation point of a circular cylinder placed normal to the flow. Bıyıklıoğlu, Tahir; Department of Mechanical Engineering (1971)
Theoretical investigation of conjugate condensation heat transfer inside vertical tubes Köse, Serhat; Yeşin, Ahmet Orhan; Department of Mechanical Engineering (2010) Based on the well-known theoretical studies related to the film condensation inside vertical tubes, a known temperature distribution is prescribed as boundary condition at the inner surface of the tube wall. But, in reality, there is a thermal interaction between the condensate fluid and conduction through the wall where the temperature variation along the inner surface of the tube wall is unknown and this unknown temperature profile should be determined by taking account of this interaction. In other words...
Theoretical calculation of the effect of free stream turbulence on heat transfer in the vicinity of stagnation point of a circular cylinder for different prandtl numbers. Alayıoğlu, Hamdi; Department of Mechanical Engineering (1970)
Theoretical analysis of the tube drawing process and design of a tube drawing bench. Yücel, Yavuz M; Department of Mechanical Engineering (1974)

Citation Formats

I. Yeğen, “Theoretical investigation of effects of channel walls on the pressure, lifts, and moment coefficients of a thin airfoil in a straight channel.,” Middle East Technical University, 1971.