Acoustic measurements of three Prop-Fan models-Reference-Cited by-同舟云学术

Acoustic measurements of three Prop-Fan models

Published:1980-06-04 Issue: Volume: Page:
ISSN:
Container-title:6th Aeroacoustics Conference
language:
Short-container-title:

Author:

BROOKS B.¹

Affiliation:

1. United Technologies Corp., Hamilton Standard Div., Windsor Locks, Conn.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-995

Reference16 articles.

1. l.Black,D.M.;Menthe,R.W.;andWainauski,H.S.: Aerodynamic Design and Performance Testing of an Advanced 30"Swept,Eight BladedPropeller at Mach Numbersfrom 0.2to 0.85.NASACR-3047,1978.

2. Jeracki, R.J.; etal: Wind Tunnel Performance of Four Energy EfficientPropellers DesignedforMach 0.8Cruise, NASATM 79124,1979.

3. Metzger, F.B.; Rohrbach,C.: Aeroacoustic Design of the Prop-Fan. AIAA 79-0610,1979.

4. Dittmar, J.H.; et, al: ToneNoiseofThreeSupersonic Helical TipSpeed Propellers in aWind Tunnel,NASA TM79161,1979.

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