Prediction of a non-uniform freestream velocity distribution for counterrotating propeller configurations and the effect on performance/acoustics /

A methodology for predicting the performance and acoustics of counterrotating propeller configurations was enhanced by incorporating a method for computing the non-uniform freestream velocity distribution entering the propeller disc plane due to an axi-symmetric propeller spinner and airplane forebo...

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Bibliographic Details

Main Author:	Allen, Christopher Shane, 1964-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1993.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy