Active Flow Control and Its Applications in Supersonic Boundary Layer

<p id="p1">Boundary layer transition is a typical aerodynamic phenomenon in supersonic flow that refers to the transition of the boundary layer from laminar flow to turbulent flow. The instabilities and transition mechanisms are complicated. A turbulent boundary layer has an associated higher energy...

Descripción completa

Detalles Bibliográficos

Autor principal:	Tian, Gan
Formato:	Capítulo de libro
Lenguaje:	inglés
Publicado:	IntechOpen 2023
Materias:	Physical Sciences, Engineering and Technology
Acceso en línea:	https://www.intechopen.com/chapters/1146923
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!