I seriously doubt it. That said, I'll claim ignorance here because I have not studied that part of things in depth. I know that it can take a lot to break-up the boundary layer in any meaningful way. In aircraft design there are reasons having nothing to do with heat transfer to want to break-up the boundary layer. As I understand it this can be difficult to achieve across a large surface (I'm assuming at sub-sonic speeds, don't know). They even resort to such devices as drilling small holes and literally sucking the boundary layer from the surface. This problem is tougher than it might seem. I am not an aero guy, I've learned a lot from thousands of hours dedicated to finding solutions to our specific problems, but I am far from an expert. Maybe an aero expert on HN can fill-in some of the holes.
At some level, think about it this way: At some point, microscopic as it might be, some of the air molecules touching the fins have to "stick" to the surface of the fins. At that point air molecule velocity with respect to the fin surface is zero. Then there are molecules that stick to these molecules one layer above, and so on. After a certain thickness the greater airflow will win out and molecules will move at the average velocity of the bulk air mass moving across the fins. What you have is a velocity profile from zero to the average air mass velocity. That's your boundary layer. You can do things to make it thinner, but eliminating it is very difficult. Techniques like impingement cooling do this to varying degrees of efficiency.
At some level, think about it this way: At some point, microscopic as it might be, some of the air molecules touching the fins have to "stick" to the surface of the fins. At that point air molecule velocity with respect to the fin surface is zero. Then there are molecules that stick to these molecules one layer above, and so on. After a certain thickness the greater airflow will win out and molecules will move at the average velocity of the bulk air mass moving across the fins. What you have is a velocity profile from zero to the average air mass velocity. That's your boundary layer. You can do things to make it thinner, but eliminating it is very difficult. Techniques like impingement cooling do this to varying degrees of efficiency.