LIC (version 0.0.2)

airfoil: Airfoil self-noise

Description

The Airfoil self-noise data set

Usage

data("airfoil")

Format

A data frame with 1503 observations on the following 6 variables.

V1

a numeric vector

V2

a numeric vector

V3

a numeric vector

V4

a numeric vector

V5

a numeric vector

V6

a numeric vector

Details

The data set contains 1503 data points, including the 6 variables. Among them, the scaled sound pressure level is the dependent variable and the other five are independent variables.

References

T.F. Brooks, D.S. Pope, and A.M. Marcolini. Airfoil self-noise and prediction. Technical report, NASA RP-1218, July 1989.

Examples

# NOT RUN {
data(airfoil)
## maybe str(airfoil) ; plot(airfoil) ...
# }