Investigation on sound field model of propeller aircraft - The effect of rigid fuselage boundary

Journal of Sound and Vibration

Volumn 209, Issue 2, 1998, Pages 317-328

  Wang, T Q ^a   Zhou, S ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; COMPUTATIONAL METHODS; FUSELAGES; MATHEMATICAL MODELS;

ACOUSTIC ANALOGY METHOD;

AIRCRAFT PROPELLERS;

EID: 0031672367     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1997.1231     Document Type: Article

References (13)

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3. F. FARASSAT 1980 AIAA-80-0996. A collection of formulas for calculation of rotating blade noise-compact and noncompact source results.
4. F. FARASSAT 1974 Journal of Sound and Vibration 32, 387-405. The acoustic far-field of rigid bodies in arbitrary motion.
5. B. MAGLIOZZI 1982 Journal of Aircraft 19, 104-111. Acoustic pressure on a prop-fan aircraft fuselage surface.
6. B. M. BROOKS and K. G. MACKALL 1984 AIAA 84-0250. Measurement and analysis of acoustic flight test data for two advanced design high speed propeller models.
7. W. E. ZORUMSKI 1986 NASA TM-83199 Part 3. Aircraft Noise Prediction Theoretical Manual.
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9. L. D. POPE and E. G. WILBY 1984 NASA CR-3813. Propeller aircraft interior noise model.
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11. L. N. LONG 1983 NASA TP-2191. The compressible aerodynamics of rotating blade based on acoustic formulation.
12. F. FARASSAT 1984 AIAA-84-2303. The united acoustic and aerodynamic prediction theory of advanced propellers in the time domain.
13. P. M. MORSE and K. V. INGARD 1968 New York: McGraw-Hill. Theoretical Acoustics.