Path: utzoo!utgpu!news-server.csri.toronto.edu!mailrus!cs.utexas.edu!samsung!zaphod.mps.ohio-state.edu!tut.cis.ohio-state.edu!att!cbnews!military Newsgroups: sci.military Subject: Ducted Fan Sub props Message-ID: <1990Jun6.142332.5428@cbnews.att.com> Date: 6 Jun 90 14:23:32 GMT Sender: military@cbnews.att.com (William B. Thacker) Distribution: na Organization: AT&T Bell Laboratories Lines: 32 Approved: military@att.att.com From: att!jsugate!nak We just had this discussion under another guise about a month ago - Status: R remember the bypass ratio turbine discussions? The final word I heard was that for maximum thrust, move a lot of air at a lesser speed. This is why the turbofan engines have such huge diameters. As far as the ducted prop enlarging the sub envelope too greatly, there is another answer - don't enclose the prop in the main hull of the sub: (poor diagrams follow) _ _ __ ___/ \________ __/ \________/ \ ( \-/ | ( | || |-/| <- fins at back (______________/-\__| (____________| || |-\| \__/ ^ ^ | | ducted fan large, solid center ring Put the ducted fan at the rear end. We can get the diameter needed for good efficiency without growing the sub in diameter. For a really big diameter, make the fan a ring around the sub since the center of the fan contributes least to the thrust (less area) Besides, from what I've read of Seawolf proposals in the press, the expanded diameter (forty feet?) is a great advantage for the design compared to the Los Angeles class. Much less cramped, more interior volume. Neil Kirby ...att!jsugate!nak