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Volumn 36, Issue 5, 1998, Pages 783-790

Development of an improved Kirchhoff method for jet aeroacoustics

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EID: 0342453317     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.437     Document Type: Article
Times cited : (30)

References (28)
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  • 2
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  • 7
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    • A New Boundary Integral Formulation for the Prediction of Sound Vibration
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  • 8
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    • American Helicopter Society, Alexandria, VA
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  • 10
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    • Lighthill, M.J.1
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    • Discontinuities in Aerodynamics and Aeroacoustics: The Concept and Applications of Generalized Functions
    • Farassat, F., "Discontinuities in Aerodynamics and Aeroacoustics: The Concept and Applications of Generalized Functions," Journal of Sound and Vibration, Vol. 55, No. 2, 1977, pp. 165-193.
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  • 15
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    • On the Applicalion of the Kirchhoff Formula for Moving Surfaces
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  • 17
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    • The Uses and Abuses of the Acoustic Analogy in Helicopter Rotor Noise Prediction
    • Farassat, F., and Brentner, K. S., "The Uses and Abuses of the Acoustic Analogy in Helicopter Rotor Noise Prediction," Journal of the American Helicopter Socity, Vol. 33, No. 1, 1988, pp. 29-36.
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    • Farassat, F.1    Brentner, K.S.2
  • 19
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    • Structure of Supersonic Jet Flow and Its Radiated Sound
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  • 25
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  • 26
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.