In 1971, the US National Aeronautics and Space Administration (NASA) published a
seminal report—NASA SP-8072—which compiled the results of the early supersonic jet …

The Reynolds number effect on the aeroacoustic fields of a supersonic jet was
experimentally investigated via particle image velocimetry (PIV), schlieren visualization, and …

A quantitative assessment of the acoustic source field produced by a laboratory-scale
heated jet with a gas dynamic Mach number of 1.55 and an acoustic Mach number of 2.41 is …

Application of phased-array algorithms to acoustic measurements in the vicinity of a high-
performance military aircraft yields equivalent source reconstructions over a range of engine …

Although near-field acoustical holography (NAH) and acoustic intensity analysis have
previously been used to investigate the apparent jet noise sources produced by military …

Complex-valued functions are often separated into real and imaginary values. For functions
that demonstrate periodicity, a separation into magnitude and phase values is often more …

View Video Presentation: https://doi. org/10.2514/6.2023-3351. vid This paper describes
investigations into convective Mach number and its relationship to maximum radiation angle …

This letter describes how a landmark 1960s supersonic jet noise experiment influenced
subsequent noise models. A discrepancy in other researchers' application of Potter and …

The noise emanating from the exhaust of high speed military aircraft affects the hearing and
performance of the crew working in close proximity to the aircraft. Moreover, jet noise is also …

In the field of supersonic jet noise, measurements of full-scale afterburning jet engines are
infrequent and provide unique opportunities to better understand jet noise phenomena. This …