Work

Effects of Surface Roughness on Pressure Distribution and Boundary Layer Over Compressor Blades at High Reynolds Number in a Two-Dimensional Cascade.

Year: 1985

Type: article

Source: Defense Technical Information Center (DTIC)

Author: Lawrence E. Williams

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W1516441284

FWCI:

Cites:

Cited by: 1

Related to: 10