Work

Two-dimensional cascade test of a highly loaded, low-solidity, tandem airfoil turbine rotor blade

Year: 1973

Type: article

Abstract: A tip region section of a low-solidity tandem airfoil blade for a turbine rotor was tested in a two-dimensional cascade tunnel at solidities of 0.736 and 0.912. Blade surface static pressures and blade exit total and static pressure and flow angle were surveyed. Blade surface velocities, wake shapes, and kinetic energy losses were analyzed and compared with values for 1.852 solidity tandem airfoil blading.

Source: NASA STI Repository (National Aeronautics and Space Administration)

Authors: J Kline, R. G. Stabe

Institution: Glenn Research Center

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: green

OpenAlex ID: W345174696

FWCI:

Cites: 1

Cited by: 1

Related to: 10