Path: utzoo!utgpu!news-server.csri.toronto.edu!rpi!zaphod.mps.ohio-state.edu!samsung!uunet!lhdsy1!yzarn From: yzarn@lhdsy1.chevron.com (Philip Yzarn de Louraille) Newsgroups: rec.skydiving Subject: Re: Skydiving at supersonic airspeeds Message-ID: <996@lhdsy1.chevron.com> Date: 24 Jun 91 17:06:13 GMT References: <1991Jun24.135815.8781@cc.curtin.edu.au> Organization: Chevron Oil Field Research, La Habra, CA. Lines: 59 In article <1991Jun24.135815.8781@cc.curtin.edu.au> tcliftonr@cc.curtin.edu.au writes: >In the discussions arising from >GRAPH OF OSC'N DUE TO HIGH WINDFORCE > >Walter@cayman.AMD.COM (Walter Butler) writes: > > >>It is possible that the jumper ( at 750 mph and 1.6 gees of >>drag after a 120 000 ft exit) will have stability problems >>from the supersonic airflow. Don't let the term "supersonic" affect you too much. If a skydiver was going supersonic at low altitude, *that* would be something to write about, but going supersonic at high altitude is nothing to scream about. > >Because of the soft impact with the atmosphere there will be >an extended period of 30 seconds or so of deceleration, where >much more wind force is available to induce "rocking" in a >normally utterly stable skydiver. (A non skydiver is likely >to go further, into a tumble, and a spin is also likely) Intuitively, I disagree. > > >>I am no expert, but believe that the shockwaves can cause >>very localized areas of high stress and drag. The skydiver will go fast but the atmosphere will be tenuous, so why shockwaves? Airplanes experience shockwaves but they have *engines*, skydivers don't. > >It sure would. Perhaps some of your NASA colleagues - the re- >entry people - might know enough of the physics. Perhaps they >already have a re-entry simulator. As it stands, this >(subsonic) simulator is extrapolated out of its proven valid >range. Ha! As it stands, what is the range of the simulator? (what is its maximum altitude?) > >In particular, we need to know how the drag coefficient (for >us brick-shapes) changes for low supersonic flight. Then we >need to know the effect of temperature on the drag >coefficient. Certainly the stratospheric cold of -56 degrees >affects viscosity and reduces drag. > >For vibrations and oscillations, we need to know the effect of >the compression cones on the extremities and how long they >take to build up. Vibrations, vibrations? Hey, we are made of soft (living) tissue, not rigid metal. Nor are we hollow, unlike most airplanes. > >Let's salute their first exploration of impact. Whatever >they find out for us, it is going to be interesting. Agreed. -- Philip Yzarn de Louraille Internet: yzarn@chevron.com Research Support Division Unix & Open Systems Chevron Information & Technology Co. Tel: (213) 694-9232 P.O. Box 446, La Habra, CA 90633-0446 Fax: (213) 694-7709