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On Wed, 07 Jul 2004 17:54:59 +0000, Mike Rapoport wrote:
Gee what do you think the indicated airspeed is at M.85 at FL350? It looks like the calibrated[0] airspeed is around 325mph: https://ewhdbks.mugu.navy.mil/mach-as.htm I seem to remember that Mach 0.85 is transonic, so air is actually flowing at supersonic speeds over some parts of the airplane (nose, wings, tail?) and subsonic over others. All kinds of stuff that I don't know how to predict happens then. Maybe someone here is an aerodynamicist who has a better feel for compressible flow? But, *that* is why I am skeptical of the Mythbuster's conclusion -- it seems to me that supersonic/transonic airflow anywhere would be a significant consideration -- especially if the flow happens to be over the bullet-hole. -Luke [0] IIRC, "indicated" airspeed isn't valid above Mach 0.3 because of compressibility effects -- but it has been quite some time since I took that class (and I wasn't proud of my grade) so I could be very wrong. I have just enough education on the topic to appreciate the expertise of people who actually know what they're talking about! |
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I forget the exact numbers but the dynamic preasure on the nose of an jet
aircraft at cruise is about 9psi above ambient. Anyway, anybody who has ever seen pictures of shot-up military aircraft can see that the airflow didn't cause the skins to tear. Mike MU-2 "Luke Scharf" wrote in message news ![]() On Wed, 07 Jul 2004 17:54:59 +0000, Mike Rapoport wrote: Gee what do you think the indicated airspeed is at M.85 at FL350? It looks like the calibrated[0] airspeed is around 325mph: https://ewhdbks.mugu.navy.mil/mach-as.htm I seem to remember that Mach 0.85 is transonic, so air is actually flowing at supersonic speeds over some parts of the airplane (nose, wings, tail?) and subsonic over others. All kinds of stuff that I don't know how to predict happens then. Maybe someone here is an aerodynamicist who has a better feel for compressible flow? But, *that* is why I am skeptical of the Mythbuster's conclusion -- it seems to me that supersonic/transonic airflow anywhere would be a significant consideration -- especially if the flow happens to be over the bullet-hole. -Luke [0] IIRC, "indicated" airspeed isn't valid above Mach 0.3 because of compressibility effects -- but it has been quite some time since I took that class (and I wasn't proud of my grade) so I could be very wrong. I have just enough education on the topic to appreciate the expertise of people who actually know what they're talking about! |
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On Wed, 07 Jul 2004 20:21:51 +0000, Mike Rapoport wrote:
I forget the exact numbers but the dynamic preasure on the nose of an jet aircraft at cruise is about 9psi above ambient. ~9psi doesn't sound too bad. I'd buy that that the skin would stay together with that number. I'm still curious to see if any sort of shockwave-like thing from a the transonic flow over a bullethole would do any extra damage. Also, someone recently was telling me that a supersonic wind-tunnel (up to Mach 3, I believe) that they use works on 50psi -- but the system maintains 50psi over a large area and pushes the air through a *much* smaller throat... Anyway, anybody who has ever seen pictures of shot-up military aircraft can see that the airflow didn't cause the skins to tear. Yes, but they're built with the expectation that they'll be shot at. I'd probably put a thicker skin on an airplane that was designed for civilian use. I've heard stories about midair collisions where the wing of a jet fighter literally sliced the wing of another aircraft off (with minimal damage to the wing). But, at only 9psi above ambient pressure, I'd buy that the skin would stay together. But I wouldn't want to actually try it without some rigorous testing! -Luke |
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"Luke Scharf" wrote in message I seem to remember that Mach 0.85 is
transonic, so air is actually flowing at supersonic speeds over some parts of the airplane (nose, wings, tail?) and subsonic over others. M.85 is called the transonic region, however, most airliners are designed to cruise at a speed just below that speed where shock waves start to form. Cruising with shock waves burns a whole lot of fuel. In the B-727, we normally cruised at .77 unless it was the last leg of the week and we wanted to catch a jumpseat home. Then we bumped it up to .88. At M.88, the shockwaves coming off the square corners of the windscreen were so loud, we couldn't converse with one another. We burned a bunch of extra fuel too. In the MD-80, we normally cruise at M.76. We can bump it up, but at .81, the rumble of shockwaves on the wings is disconcerting to the passengers. We burn 6% more fuel just to go 10 or 12 knots faster. In contrast, the B-747 cruises at M.84 without forming shockwaves. It is designed that way. But, *that* is why I am skeptical of the Mythbuster's conclusion -- it seems to me that supersonic/transonic airflow anywhere would be a significant consideration -- especially if the flow happens to be over the bullet-hole. Jetliners don't use thin .020" sheet aluminum for structural parts as you would find in a Cherokee or Skyhawk. Shockwaves over a bullet hole are insignificant. What is significant is when a force is strong enough to cause some sheet metal to expand into the airstream and the airstream peels it backwards. Then structural integrity is compromised, often catastrophically. D. |
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uuuuhhhh,
What about that Hawaiian Air 737 that went "convertable" mid flight and landed relatively intact? What about the scores of military cargo aircraft that have been shot up and still seem to stay together (not too structurally different, and made by the lowest bidder!!!) Hell, even the DHL A320 took a hit by a MANPAD and made it back... "Luke Scharf" wrote in message news ![]() On Wed, 07 Jul 2004 16:37:56 +0000, Casey Wilson wrote: The guys sealed up a junked out cabin, pressurized it, then fired 9mm bullets through first the skin and then a window. Nothing exciting happened. Pretty interesting stuff. One factor that they neglected to account for is that many airliners fly at speeds approaching Mach 0.85. I'd have to see a section of aluminum skin with a bullet-hole in it staying intact in a transonic wind-tunnel that was running about that speed before I put much stock in their results. -Luke |
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![]() "Mark T. Mueller" wrote in message ... What about the scores of military cargo aircraft that have been shot up and still seem to stay together (not too structurally different, and made by the lowest bidder!!!) The military hasn't bought aircraft that way in a very long time. |
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Subject: Mythbusters and explosive decompression
From: Luke Scharf One factor that they neglected to account for is that many airliners fly at speeds approaching Mach 0.85. I'd have to see a section of aluminum skin with a bullet-hole in it staying intact in a transonic wind-tunnel that was running about that speed before I put much stock in their results. Luke you must not of seen many combat acft return home with holes big enough to park a V W in. Mac USAF retired |
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On Thu, 08 Jul 2004 19:01:59 +0000, Mackfly wrote:
Luke you must not of seen many combat acft return home with holes big enough to park a V W in. Mac USAF retired How fast did they fly home? Also, how thick is the skin on a combat aircraft compared to a civilian airliner? I'll buy that the aircraft could stay together. The Mythbusters simulation wasn't very comprehensive... But, then again, I know just enough about high-speed aerodynamics to be afraid! :-) -Luke |
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My conviction of the miniscule damage to be caused by a sky
marshall or pilot popping off a few caps at a terrorists has been reinforced. Some years ago an airliner landed here in Richmond after having been shot by someone on the ground. It was a completely coincidental thing where someone shot into the sky and just happened to hit an airliner. The news report showed the bullet hole; other than that the plane was fine. |
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If a bullet penetrated the skin of an aircraft, the plane could not have
been more than a couple of thousand feet high, and it would not be pressurized. "John Harlow" wrote in message ... My conviction of the miniscule damage to be caused by a sky marshall or pilot popping off a few caps at a terrorists has been reinforced. Some years ago an airliner landed here in Richmond after having been shot by someone on the ground. It was a completely coincidental thing where someone shot into the sky and just happened to hit an airliner. The news report showed the bullet hole; other than that the plane was fine. |
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