Two dimensional nonlinear analysis of sound transmission through a near-sonic throat flowA two-dimensional nonlinear theory of sound transmission through a nonuniform duct carrying a near-sonic throat flow is described. The mean flow in the duct is treated according to a generalized quasi-one dimensional model, and the analysis of the unsteady perturbations is carried out using the Method of Matched Asymptotic Expansions. The linearized acoustic field in the subsonic regions of the duct is approximated by a Wave Envelope model which is matched asymptotically with a nonlinear inner solution valid in the near-sonic throat region. Numerical results are presented to illustrate the predictions of the theory. It is found that, in general, shock waves develop in the acoustic field during transmission through the near-sonic flow. Unlike previous one-dimensional theories, the current study shows that dispersion can play a major role in the propagation process.
Document ID
19840035343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, M. K. (Joint Inst. for Advancement of Flight Sciences Hampton, VA, United States)
Uenishi, K. (Joint Institute for Advancement of Flight Sciences Hampton, VA, United States)