Abstract
Static run-up and flyover measurements of a high-performance military aircraft were conducted at Edwards Air Force Base, CA, as part of a joint program among Wyle Laboratories, The Pennsylvania State University, and The University of Alabama to develop better noise models for military aircraft. This paper describes the measurement program and the resulting acoustic data. These measurements clearly demonstrate nonlinear source and propagation effects from military jet aircraft. Moreover, these results serve as a comparative data set for the evaluation of propagation models. [Work is supported by the Strategic Environmental Research and Develop Program.]
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