Amplitude Method of Laminar-Turbulent Transition Prediction in Three Dimensional Supersonic Boundary Layer at Swept Wing Boundary Layer Control, High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Aerodynamics, Transition to Turbulence, Turbulence Modeling and SimulationBy tverminOctober 26, 2023Maksim V. Ustinov DOI Number XXX-YYY-ZZZ Conference Number HiSST 2018_19601030
