4th Aeroacoustics Conference 1977
DOI: 10.2514/6.1977-1322
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Noise generation by turbulence interaction with a rotor

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1978
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1978
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“…Incorporation of blade-to-blade correlation of unsteady lift into Sevik's analysis is presented in the following. Consider the aerodynamic frequency response functions of equation (5). The subscript on this function refers to a particular spanwise element of a propeller blade and the summation is over all spanwise elements.…”
Section: A Theory To Include Blade-to-blade Correlation Effectsmentioning
confidence: 99%
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“…Incorporation of blade-to-blade correlation of unsteady lift into Sevik's analysis is presented in the following. Consider the aerodynamic frequency response functions of equation (5). The subscript on this function refers to a particular spanwise element of a propeller blade and the summation is over all spanwise elements.…”
Section: A Theory To Include Blade-to-blade Correlation Effectsmentioning
confidence: 99%
“…The functions, Gh91l(w) and GhQ22(w), are defined in equation (5). Substituting these expressions for Ghgll() and Gh22(w) into equation (11) results in…”
Section: A Theory To Include Blade-to-blade Correlation Effectsmentioning
confidence: 99%