- #1
scott_alexsk
- 336
- 0
Hello,
In some papers I have come across this term. There are no formal definitions online, but I have a rough idea that it deals with a change in the nature of air in the boundry layer of an aircraft surface after reaching supersonic speeds. About this topic I have several questions. What is the formal defintion of the shock boundry layer? Also does anyone know anything about a responsive aircraft surface to variable speeds?
Thanks,
-scott
In some papers I have come across this term. There are no formal definitions online, but I have a rough idea that it deals with a change in the nature of air in the boundry layer of an aircraft surface after reaching supersonic speeds. About this topic I have several questions. What is the formal defintion of the shock boundry layer? Also does anyone know anything about a responsive aircraft surface to variable speeds?
Thanks,
-scott