The acoustic noise generated by the rotate point source, UH-1H rotor in hover and AH-l/OLS in forward flight were calculated, and the computed results from several methods were compared with each other and with the experimental data.
英
美
- 采用旋轉點(diǎn)源、UH-1H懸停旋翼、AH-1/OLS前飛旋翼作為算例,對所采用的各種噪聲預測方法進(jìn)行了比較。