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Underexpanded Supersonic Jets from Elliptical Nozzle with Aft Deck

机译:椭圆形喷嘴和后甲板的超音速超音速喷气机

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An experimental investigation of an underexpanded supersonic jet issuing from a circular nozzle, an ellipticalnozzle, and an elliptical nozzle with an aft deck at different nozzle pressure ratios (NPRs) is reported in this paper.Static-pressure measurements over the nozzle walls were analyzed to understand the internal flow structure.Schlieren visualization and conical probe measurements were conducted to elucidate the development of the jetsissuing from the nozzles. The sound-pressure level in the near field was measured, and it was found that the screechamplitudes were 26 dB lower in the elliptical nozzle with an aft deck. The screech-tone frequencies were observed tobe above and near audible region (16 kHz) in the presence of the aft deck at NPRs 3 and 4. The jets emanating fromthe circular and truncated elliptical nozzles were observed to be flapping about the jet axis at NPRs 3 and 4. Theunsteadiness of the jet was reduced by locking the jet onto the aft deck. The centerline Mach-number decay revealedthat, due to the screeching effect, the truncated elliptical nozzle has a shorter potential core length and larger jetspreading. The flow separation and reattachment were observed over the aft-deck surface for higherNPRconditions.
机译:本文报道了由圆形喷嘴,椭圆形喷嘴和带有尾板的椭圆形喷嘴在不同的喷嘴压力比(NPRs)下产生的超音速超音速喷射的实验研究。了解了内部流动结构。进行了Schlieren可视化和锥形探针测量,以阐明从喷嘴喷出的射流的发展。测量了近场中的声压级,发现在带有后甲板的椭圆形喷嘴中,其振幅降低了26 dB。在NPR 3和4处,在船尾甲板存在的情况下,可以观察到尖音频率在听觉区域的上方和附近(16 kHz)。观察到从圆形和截头椭圆形喷嘴喷出的射流在NPR处围绕射流轴拍动。参照图3和图4。通过将喷射器锁定在船尾甲板上来减少喷射器的不稳定。中心线马赫数衰减表明,由于产生尖锐的挤压效应,截断的椭圆形喷嘴具有较短的潜在核心长度和较大的喷射展宽。对于较高的NPR条件,在船尾甲板表面观察到了流动分离和重新附着。

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