This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.
|Journal||Journal of Physics: Conference Series|
|Publication status||Published - 6 Dec 2019|
|Event||16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 - Novosibirsk, Russian Federation|
Duration: 30 Sep 2019 → 5 Oct 2019