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A ray tracing approach to calculate acoustic shielding by the silent aircraft airframe

Agarwal, A. (författare)
Dowling, A. P. (författare)
Shin, H. -C (författare)
visa fler...
Graham, W. (författare)
Sefi, Sandy (författare)
KTH,Numerisk Analys och Datalogi, NADA
visa färre...
 (creator_code:org_t)
2006
2006
Engelska.
Ingår i: Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference. - 1563478099 - 9781563478093 ; , s. 2799-2818
  • Konferensbidrag (refereegranskat)
Abstract Ämnesord
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  • The Silent Aircraft is in the form of a flying wing with a large wing planform and a propulsion system that is embedded in the rear of the airframe with intakes on the upper surface of the wing. Thus a large part of the forward-propagating noise from the intake ducts is expected to be shielded from observers on the ground by the wing. Acoustic shielding effects can be calculated by solving an external acoustic scattering problem for a moving aircraft. In this paper, acoustic shielding effects of the Silent Aircraft airframe are quantified by a ray-tracing method. The dominant frequencies from the noise spectrum of the engines are sufficiently high for ray theory to yield accurate results. It is shown that for low-Mach number homentropic flows, a condition satisfied approximately by the Silent Aircraft during take-off and approach, the acoustic rays propagate in straight lines. Thus, from Fermat's principle it is clear that classical Geometrical Optics and Geometrical Theory of Diffraction solutions are applicable to this moving-body problem as well. The total amount of acoustic shielding at an observer located in the shadow region is calculated by adding the contributions from all the diffracted rays (edge-diffracted and creeping rays) and then subtracting the result from the incident field without the airframe. Experiments on a model-scale geometry have been conducted in an anechoic chamber to test the applicability of the ray-tracing technique. The three-dimensional ray-tracing solver is validated by comparing the numerical solution with analytical high-frequency asymptotic solutions for canonical shapes.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Strömningsmekanik och akustik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Fluid Mechanics and Acoustics (hsv//eng)

Nyckelord

Acoustic shielding
Acoustic shielding effects
Noise propagation
Silent aircraft airframe
Acoustic wave propagation
Aircraft propulsion
Airframes
Embedded systems
Numerical methods
Ray tracing
Wings
Noise abatement

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Av författaren/redakt...
Agarwal, A.
Dowling, A. P.
Shin, H. -C
Graham, W.
Sefi, Sandy
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TEKNIK OCH TEKNOLOGIER
TEKNIK OCH TEKNO ...
och Maskinteknik
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