Nickul18
New member
- Mar 21, 2006
- 6
Ok , we've been testing a simple convergent nozzle operating at pressure ratios of approxomately 3-4 (To, approx 200C)exhausting into static free air, and we are experiecing some pretty elevated levels of noise. We expected this but the question really is what is the source of the noise? Is it the shearing of the jet boundary ?? or some have said the shock structure itself generates pressure perturbations. Anybody have any ideas ??