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Keywords: velocity
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Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2003, 125(3): 598–606.
Published Online: August 27, 2003
..., an optimization procedure was developed to determine the principal dimension of the rotor. The mean relative velocity in the rotor passages in the direction of the flow would be accelerated but flow velocity on the blade surfaces experiences a significant space rate of deceleration. The rate of deceleration can...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. October 2002, 124(4): 665–669.
Published Online: November 7, 2002
... Turbine and Aeroengine Congress and Exhibition, Amsterdam, The Netherlands, June 3-6, 2002. Manuscript received by the IGTI, April 10, 2001. Paper No. 2002-GT-30238. Review Chair: E. Benvenuti. 10 April 2001 07 11 2002 gas turbines boundary layer turbulence vortices velocity...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2002, 124(2): 176–186.
Published Online: April 9, 2002
... numbers from about 4 × 10 5 to 10 6 . The measurements include the midspan losses, blade loadings and base pressures. In addition, the axial-velocity-density ratio (AVDR) was extracted for each operating point. The AVDR was found to vary from about 0.98 at −10.0 deg of incidence to about 1.27 at +14.5 deg...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2002, 124(1): 107–118.
Published Online: February 1, 2001
... velocities on the pressure and suction surfaces. Although the mean velocity profiles appeared to be more consistent with laminar profiles, large velocity fluctuations were measured in the boundary layer along the pressure side at the high freestream turbulence conditions. Along the suction side, transition...
Journal Articles
Publisher: ASME
Article Type: Technical Briefs
J. Turbomach. July 2000, 122(3): 587–588.
Published Online: October 1, 1997
... turbulence laminar to turbulent transitions friction velocity momentum The mean velocity ( U ) distribution, and the skin friction coefficient C f in the linear-combination model of Dhawan and Narasimha 4 are: (1) U lc = 1 − γ U L + γ U T...