Recent content by Harmonic

Thanks for your reply random guy. Just to clarify, I wasn't suggesting that I'd use a uniform span load distribution, because then why use a VLM code at all! I understand that the effect of the shock will not be the same everywhere on the wing, but I was thinking this might not be too bad a...

Hi, I'm looking for an aerodynamic code to model a transonic (say around M=0.8) wing for some basic structural sizing and performance estimation. I'm hoping to use the MATLAB based VLM code Tornado. It has an inbuilt Prandtl-Glauert correction option. I realize that this is technically...