Xref: utzoo sci.military:10739 rec.models.rockets:2331 Path: utzoo!utgpu!news-server.csri.toronto.edu!cs.utexas.edu!sdd.hp.com!zaphod.mps.ohio-state.edu!samsung!olivea!oliveb!veritas!amdcad!amdcad!military From: d9bertil@dtek.chalmers.se (Bertil Jonell) Newsgroups: sci.military,rec.models.rockets Subject: Re: Secant Ogive Message-ID: <1991Jun18.074409.14983@amd.com> Date: 17 Jun 91 15:53:50 GMT References: <1991Jun13.055308.22899@amd.com> <1991Jun14.080300.20680@amd.com> <1991Jun15.021629.309@amd.com> Sender: military@amd.com Organization: Chalmers University of Technology, Gothenburg, Sweden Lines: 14 Approved: military@amd.com From: d9bertil@dtek.chalmers.se (Bertil Jonell) weverka@spot.Colorado.EDU (Robert T. Weverka) writes: >I have considered, but not implemented: >means of bringing air into the wake region from rocket side wall or nose. Has been done for artillery projectiles. It's called Base bleed, and consists of a small, relatively slow burning, powder charge. The gases from it are expelled from the bottom of the shell and this slight overpressure will reduce the overall drag of the shell. -bertil-