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#1
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Greg Arnold wrote:
When you are cruising at 20,000' to 30,000', doesn't the effect of altitude cause IAS to be substantially less than ground speed? That is indeed true. However, there are aeroelastic concerns (such as flutter) which may result in a lower indicated vne at high altitude. Charles |
#2
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"Charles Crosby" wrote in message
... Greg Arnold wrote: When you are cruising at 20,000' to 30,000', doesn't the effect of altitude cause IAS to be substantially less than ground speed? That is indeed true. However, there are aeroelastic concerns (such as flutter) which may result in a lower indicated vne at high altitude. Charles http://home.comcast.net/~johan.larso...ride-home.html The Long Ride Home Harold Peterson This article originally appeared in the August 1, 1966 issue of Sports Illustrated. David Stevenson provided the issue of SI for scanning. ' "We're plagued with people who want to emphasize the danger," George said. "Just flying a sailplane around is safer than power flying. One fundamental safety factor is the soft landing. You have marvelous control-anywhere between a 40 degree approach with full dive breaks to 3 degrees with none. In contest or record flight, of course, you're definitely stretching a little. On a glide you may easily reach 150 mph where the placard speed is listed at 86." Placard speed is that beyond which the manufacturer makes no guarantee that things will not start coming off. ' [Quoting George Moffat. G.T.] -- Geoff The Sea Hawk at Wow Way d0t Com remove spaces and make the obvious substitutions to reply by mail When immigration is outlawed, only outlaws will immigrate. |
#3
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Soarin Again wrote:
At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. Marc |
#4
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Marc Ramsey wrote:
Soarin Again wrote: At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. If the 4DM follows the protocol used by the Duo (for which I have a manual), Vne is IAS up to approximately 2500M altitude, then the equivalent TAS from there up. If Vne for the 4DM is 275 km/hr, the TAS limitation would be around 310 km/hr. |
#5
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![]() Marc Ramsey wrote: Marc Ramsey wrote: Soarin Again wrote: At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. If the 4DM follows the protocol used by the Duo (for which I have a manual), Vne is IAS up to approximately 2500M altitude, then the equivalent TAS from there up. If Vne for the 4DM is 275 km/hr, the TAS limitation would be around 310 km/hr. The Vne for the Nimbus 4DM is 285km/h (154 kt). Flutter speeds do not follow TAS, but actually follow approximately 3/4 the way between IAS and TAS. So it is possible to fly safely past 300km/h at altitude. |
#6
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I do remember reading something a little while back on the SH website
about them having modifed a Nimbus 4 for high altitude record flights in Argentina. If I recall correctly they did modifications (probably some mass balancing) to counter the onset of flutter as a result of high TAS at altitude. Markus |
#7
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Marc Ramsey wrote:
Soarin Again wrote: At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. I find these sorts of discussions amusing. Do F1 drivers religiously follow redline engine speeds or anticipated braking limits for conditions when they're out to beat the next guy? Breaking records in aircraft is not analogous to driving the family SUV to the mall, or the 1-26 around a silver distance triangle. Speed limits and safe and reasonable don't apply. If it wasn't pushing the envelope, we'd all be doing it. My $ 0.02. Shawn |
#8
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![]() Shawn schreef: Marc Ramsey wrote: Soarin Again wrote: At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. I find these sorts of discussions amusing. Do F1 drivers religiously follow redline engine speeds or anticipated braking limits for conditions when they're out to beat the next guy? Breaking records in aircraft is not analogous to driving the family SUV to the mall, or the 1-26 around a silver distance triangle. Speed limits and safe and reasonable don't apply. If it wasn't pushing the envelope, we'd all be doing it. My $ 0.02. Shawn When not flying in an airworthiness glider you're simply not allowed to fly at all, so no records either. That does give Americans (of which most have an experimental registrated glider) in fact an unfair advantage, but up to now no one cared. Maybe that's gonna change... |
#9
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Shawn wrote:
Marc Ramsey wrote: 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. I find these sorts of discussions amusing. Do F1 drivers religiously follow redline engine speeds or anticipated braking limits for conditions when they're out to beat the next guy? Breaking records in aircraft is not analogous to driving the family SUV to the mall, or the 1-26 around a silver distance triangle. Speed limits and safe and reasonable don't apply. If it wasn't pushing the envelope, we'd all be doing it. And that's why I think these discussions are interesting instead of amusing. What risks are they taking, and how did they determine these risks? Klaus does not seem a like a crazy man, so I suspect his risk analysis would be very enlightening. And now we know it's a modified Nimbus, so perhaps he is not taking any extra risk at all - even more interesting! I hope we hear more about the modifications and how they tested their effect. -- Eric Greenwell - Washington State, USA * Change "netto" to "net" to email me directly * "Transponders in Sailplanes" http://tinyurl.com/y739x4 * "A Guide to Self-launching Sailplane Operation" at www.motorglider.org |
#10
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To average 306 he certainly exceeded that speed for much of the flight.
I too would like to understand the mods and the risk analysis for this flight. "Marc Ramsey" wrote in message m... Soarin Again wrote: At 05:42 23 December 2006, Js wrote: 306 km/hr = 190 mph = 165 knots That is an amazing feat! Yes, it is. Anyone trying to beat that record should be certain their parachute is in good shape, as the number of wings will likely total zero. Jim Does anyone know if his Nimbus 4DM has had special modifications to increase the vne at altitude, or does he just not care about operating limitations? 306 km/hr true airspeed is 200 to 220 km/hr IAS at the 20000+ foot altitudes used for these wave flights. Some gliders do require a reduction in Vne at higher altitudes, but it isn't necessarily the case that the limitation was exceeded. Marc |
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