1981-02-01

The Development of a Flyover Noise Prediction Technique Using Multiple Linear Regression Analysis 810588

At Cessna Aircraft Company, statistical analyses have been developed to define important trends in flyover noise data. Multiple regression techniques have provided the means to develop flyover noise prediction methods which have resulted in better accuracy than methods used in the past. Regression analyses have been conducted to determine the important relationship between propeller helical tip Mach number and the flyover noise level. Other variables have been included in the regression models either because the added variable contributed to reducing the remaining variation in the model or the variable appeared to be a strong causal agent of flyover noise.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Progress Report on Propeller Aircraft Flyover Noise Research

760454

View Details

TECHNICAL PAPER

New Directions in Aircraft Propulsor Noise Research

750515

View Details

TECHNICAL PAPER

A PROPELLER SYNCHROPHASER FOR AIRCRAFT NOISE CONTROL

550186

View Details

X