Progress and trends in propeller/prop-fan noise technology
Author:
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/10.2514/6.1980-856
Reference40 articles.
1. Gutln, L.t '%tbs W Flald d a RotrtMAh-BCIPW." 1936 Zhurnnl TekhDscbeSkolfIZfkl 6, 899-909(InRusskn)TnnsLtbd as 1948 NACA TM 1195.
2. IwmlnE. A. F.! "Nolae From Prmllers wlth Ssmmetrlral Sectlone at Zero Made ngle."1931 h.u 4 TTN 605.
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1. Slipstream-induced pressure fluctuations on a wing panel;Journal of Aircraft;1989-10
2. High-speed propeller noise predictions - Effects of boundary conditions used in blade loading calculations;Journal of Aircraft;1988-02
3. Advanced turboprop wing installation effects measured by unsteady blade pressure and noise;11th Aeroacoustics Conference;1987-08-17
4. Acoustic measurements of three Prop-Fan models;6th Aeroacoustics Conference;1980-06-04
5. Subsonic transport noise;International Meeting and Technical Display on Global Technology 2000;1980-05-06
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