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Project TitleLINFLUX, 3D Linearized Unsteady Aerodynamic Analysis
Track CodeLEW-17346
Websitehttp://www.grc.nasa.gov/WWW/Acoustics/analysis/support/fantone.htm
Description

LINFLUX is a three-dimensional, linearized, unsteady aerodynamic analysis (and code) that can be applied to predict the aeroacoustic and aeroelastic responses of axial-flow turbomachinery blade rows, to aerodynamic and structural excitations.

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LINFLUX Executable and Documentation Request Key

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