The effort conducted to gather additional understanding of the complex inviscid and viscid effects existing within the passages of a three-bladed axial flow inducer operating at a flow coefficient of 0.065 is summarized. The experimental investigations included determination of the blade static pressure and blade limiting streamline angle distributions, and measurement of the three components of mean velocity, turbulence intensities and turbulence stresses at locations inside the inducer blade passage utilizing a rotating three-sensor hotwire probe. Applicable equations were derived for the hotwire data reduction analysis and solved numerically to obtain the appropriate flow parameters. Analytical investigations were conducted to predict th...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
The Reynolds stress equation, pressure strain correlation, and dissipative terms and diffusion are d...
A description of the Axial Flow Turbine Research Facility (AFTRF) being built at the Turbomachinery ...
A study of the boundary layer and turbulence characteristics inside the passages of an axial flow in...
Analytical and experimental investigations of the characteristics of three dimensional turbulent bou...
The measurement and prediction is reported of three dimensional flow fields in an axial flow inducer...
Because of the long and narrow passages between the blades of a rocket pump inducer, major effects f...
Three bladed inducer and boundary layer measurements inside rotating helical blad
This paper describes an investigation of the flows in unshrouded and shrouded inducers which are kno...
The flow processes in rocket pump inducers are summarized. The experimental investigations were carr...
Axial flow pump runners known as inducers are subject to complex internal flows and fluid-induced la...
This paper describes an investigation of the flows in unshrouded and shrouded inducers which are kno...
The paper describes the results of an experimental campaign performed on a three bladed axial induce...
The characteristics of a rocket pump inducer are discussed. The effect of the pumping requirements o...
January, 1980This is part 1. Part 2 issued as his Asymmetric inlet flows through axial compressors,...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
The Reynolds stress equation, pressure strain correlation, and dissipative terms and diffusion are d...
A description of the Axial Flow Turbine Research Facility (AFTRF) being built at the Turbomachinery ...
A study of the boundary layer and turbulence characteristics inside the passages of an axial flow in...
Analytical and experimental investigations of the characteristics of three dimensional turbulent bou...
The measurement and prediction is reported of three dimensional flow fields in an axial flow inducer...
Because of the long and narrow passages between the blades of a rocket pump inducer, major effects f...
Three bladed inducer and boundary layer measurements inside rotating helical blad
This paper describes an investigation of the flows in unshrouded and shrouded inducers which are kno...
The flow processes in rocket pump inducers are summarized. The experimental investigations were carr...
Axial flow pump runners known as inducers are subject to complex internal flows and fluid-induced la...
This paper describes an investigation of the flows in unshrouded and shrouded inducers which are kno...
The paper describes the results of an experimental campaign performed on a three bladed axial induce...
The characteristics of a rocket pump inducer are discussed. The effect of the pumping requirements o...
January, 1980This is part 1. Part 2 issued as his Asymmetric inlet flows through axial compressors,...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
The Reynolds stress equation, pressure strain correlation, and dissipative terms and diffusion are d...
A description of the Axial Flow Turbine Research Facility (AFTRF) being built at the Turbomachinery ...