11th Fluid and PlasmaDynamics Conference 1978
DOI: 10.2514/6.1978-1122
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The exact numerical calculation of propeller noise

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Cited by 13 publications
(7 citation statements)
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“…To validate code a2, the prediction example of the forward flight propeller noise provided by Farassat and Brown [11] is selected, in which the experimental and theoretical results for overall noise, encompassing acoustic pressure time histories and spectra, are presented. Separately, Woan and Gregorek [15] presented theoretical results, including the acoustic pressure time histories and spectra, for the overall noise as well as for its thickness and loading noise components. In this paper, the acoustic pressure time history and spectrum of the overall noise at the observer point O 1 (0, 7.28 m, 0) are calculated using code a2.…”
Section: Rotor Geometry Model and Observer Point Coordinatesmentioning
confidence: 99%
“…To validate code a2, the prediction example of the forward flight propeller noise provided by Farassat and Brown [11] is selected, in which the experimental and theoretical results for overall noise, encompassing acoustic pressure time histories and spectra, are presented. Separately, Woan and Gregorek [15] presented theoretical results, including the acoustic pressure time histories and spectra, for the overall noise as well as for its thickness and loading noise components. In this paper, the acoustic pressure time history and spectrum of the overall noise at the observer point O 1 (0, 7.28 m, 0) are calculated using code a2.…”
Section: Rotor Geometry Model and Observer Point Coordinatesmentioning
confidence: 99%
“…where the loading noise, P L ' observed at time t emanating from blade element n is given by: (9) and the thickness noise, PT' is given by:…”
Section: Chapter III Approximate Acoustic Modelmentioning
confidence: 99%
“…The terms in Eqs. (9) and 10 The fundamental idea behind a strip analysis method is to calculate the performance of a three-dimensional propeller by modeling the blades as two-dimensional airfoil sections placed about a pitch-change axis. By accounting for three-dimensional effects in the calculation of the radial velocity and angle of attack distributions, twodimensional lift and drag data can be used to obtain the radial variations of thrust and torque which are integrated to obtain the total thrust and torque of the propeller.…”
Section: Chapter III Approximate Acoustic Modelmentioning
confidence: 99%
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“…High speed rotating blades have many applications in industry, including rotor, propeller, compressor, and turbine et al [1][2][3][4][5]. This kind of rotating blade has a high speed in the tip region, its loading is larger but its thickness is thinner.…”
Section: Introductionmentioning
confidence: 99%