**The file size is rather large, so I've posted it on rapidshare:
http://rapidshare.com/files/109684077/Final_Report_Aero_SR20.pdf.html**
I'm about to graduate college with an Aerospace Eng degree. Last week is finals, and graduation date is May 11th.
As some of you may remember, my Senior Design course focuses on MUAV (micro unmanned aerial vehicles); fully autonomous craft designed for the Army to carry out recon missions.
Our design is to carry the MUAV's under a much larger helicopter. The MUAV's will be attached to a 25x25x0.25" plate that will have certain points magnetized so the MUAV's will 'snap' into place. This plate poses a problem in the way of release and retrieval. It is highly possible that the MUAV will not be able to make it through the larger "mothership"'s downwash. And more over, the downwash
because of the plate directly under the plate could be so turbulent that the MUAV's couldn't even get out to the downwash. So, being the 'aerodynamics' guy in the group I was tasked with covering this aspect. I wrote some Matlab code in addition to using a professor's code, and also had some CFD done on the. I finished up my paper earlier this afternoon. I know some of you guys here might enjoy the read, so I've attached my paper along with the code for those who know Matlab and want to tinker with things.
Below is a sample of the CFD I had done on the plate. I'm really excited about my end product as are my professors. I just wanted to share with you guys here and maybe provide some 'cool' talk out of the norm lately. Keep in mind that I've never had a helicopter theory class nor have never studied it. i got a crash course this semester and enjoyed it so much I'm considering getting my Masters in the field... which would be odd since I work in Space Propulsion, lol. *shrugs*