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#11
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There is no such thing as "forward airspeed". Just Airspeed. The speed of the air over the wing is completely independent of ground reference points. If you want to use a ground reference, use GROUND SPEED. Airspeed and Groundspeed are easily confused when you try to describe things so don't take it so hard. To use your illustration, push the nose down 100 degrees from vertical, you are now slightly inverted and traveling backwards over the ground. Do you now have NEGATIVE AIRSPEED? Don't think so............. Scott But what happens when you cock up a chandelle and don't get the nose down before you loose forward airspeed? Seems like negative (or backwards) airspeed to me! 8-) Keith |
#12
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Well I have just posted the video, while I did take my time getting the aft
limit of the contorl stick it was not quite at 1 knot per second.... so I will keep that in mind for the next session.Check out the video on the Marske Pioneer IId page.! -thanks -mat "dhb" wrote in message thlink.net... One of the several FAA definitions that are involved in determining stall speeds is when the aft stick limit is reached. Another is the FIRST time the nose starts down as you are bringing the stick aft. Make sure that you do this test at the official 1 knot per second entry rate. In article , "Marske Flying Wings" wrote: I did a modest cross country in the Pioneer IId yesterday but what is most interesting was that I am exploring all of the flight envelope and yesterday was stalls. When I pulled the stick all the way back slowly I suddenly found that my airspeed had fallen to zero where I held it for quite some time and my sink rate was 100 down. And I have it on video! I did this many times although there was tendency to turn to the left since we have a left turn in the glider. The airspeed system was calibrated recently, both the airspeed instrument and the installation, however I did not do the calibration for zero airspeed... so it could be off slightly. I have posted a picture on the web site showing the airspeed near zero and will post a video shortly. http://www.continuo.com/marske/pione...%20pioneer.htm This is rather a long address so if this does not work go to our web site and find "Marske Pioneer IId" -mat I have been recording all of this on video to give some credibillity to my claims. |
#13
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"spektr" wrote in message ...
Bravo. So you are flying a glider with insufficient up elevator to cause a stall equipped with an airspeed indicator that doesn't register well on the low end of the spectrum. All wings stall when their critical angle of attack is exceeded. All wings stall when their angle of attack is beyond the limits. But don't put the tendency for flying wings to not stall viciously as an attribute of insufficient elevator. If the elevator had enough authority to hold the wing past the critical angle, nobody would have the touch fine enough to fly it. Contrasted to the brute force system of "conventional" designs, it takes very little to control the attitude of the flying wing types. A little time spent beyond the fiberglass and foam model kits might have allowed more people to experiment with things that are "interesting". The "Scimitar" design is a good example but those not interested in having to actually build never found out. |
#14
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There is no such thing as "forward airspeed".
All depends on where your point of referance is if the vector is positive or negative. All of the planes I have flown had the pitot somewhere in the front and I tend to have that stuck in my mind as the referance point. Substitute "ground speed" solar speed or what ever speed you like but da ting duz wat is duz G |
#15
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"Bill Daniels" wrote in message ... The Marske planform does eliminate the stall/spin as a likely source of accidents and, apparently, without a performance penalty. In exchange for this, it introduces another area where the pilot determined to find a way to crash can do so. Bill. Very good points made. But the Marske planform can and has entered spins. It may not be a likely outcome of a stall , but if you go to the NTSB website, look for the only Monarch crash. Jim talked this accident thru with me and they still aren't sure how the pilot did it. The pilot stalled in the pattern, spun in impacting the ground. I don't hold this against the aircraft, in fact I've had talked on the phone to Mat and Jim on several occasions about their gliders. I do like what I see and hear and I'm probably going to build a Monarch But back to the point............ It has insufficient elevator at low speeds to stall the aircraft. it has a high sink rate/drag envelope when slow that is different from most other gliders. You can train your way around these things but the premise of the discussion , non-stallability, is incorrect. Weve beaten the 0 airspeed thing to death. Scott |
#16
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I think it is important to understand that we did not build this Monarch F
and did not know where the CG was, what wing tips he had on it are not clear either. We viewed the video of the flight and a wing did drop but in less than a rotation the wing was flyiing again... but the pilot entered another. My feeling is that the pilot froze up.... as he said himself and may have pulled the stick all the way back and crossed the controls. I do feel he had a very far froward CG given his weight. If the CG is far forward the glider can be made to have a sharp break in the stall. At any rate we could not make this happen on the Current Monarch G's. I flew a Monarch F for a couple of seasons and it was not able to spin or stall.. When we were experimenting with the CG on the Pioneer IId we could get it to break on a stall if the CG was too far forward. thanks for your input. -mat "spektr" wrote in message ... "Bill Daniels" wrote in message ... The Marske planform does eliminate the stall/spin as a likely source of accidents and, apparently, without a performance penalty. In exchange for this, it introduces another area where the pilot determined to find a way to crash can do so. Bill. Very good points made. But the Marske planform can and has entered spins. It may not be a likely outcome of a stall , but if you go to the NTSB website, look for the only Monarch crash. Jim talked this accident thru with me and they still aren't sure how the pilot did it. The pilot stalled in the pattern, spun in impacting the ground. I don't hold this against the aircraft, in fact I've had talked on the phone to Mat and Jim on several occasions about their gliders. I do like what I see and hear and I'm probably going to build a Monarch But back to the point............ It has insufficient elevator at low speeds to stall the aircraft. it has a high sink rate/drag envelope when slow that is different from most other gliders. You can train your way around these things but the premise of the discussion , non-stallability, is incorrect. Weve beaten the 0 airspeed thing to death. Scott |
#17
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On Thu, 31 Jul 2003 17:27:46 UTC, "Marske Flying Wings"
wrote: : No this is where you are quite wrong! There is pleanty of up elevator on the : trailing edge of the main wing.... the air going over the top is separating : due to the high angle of attack and this makes the elevator ineffective, so : the nose lowers slightly and the glider picks up airspeed and it resumes : normal flight. Which is, effectively, exactly what he said... : "spektr" wrote in message : ... : So you are flying a glider with insufficient up elevator to cause a stall Ian |
#18
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On Fri, 1 Aug 2003 02:00:17 UTC, "Bill Daniels"
wrote: : The Marske planform does eliminate the stall/spin as a likely source of : accidents From what was posted here, it stalls fine but as a mushing stall (which is exactly what I get in a K8). Just as a matter of interest, what happens in a Marske if you stall it and then kick in a bootful of rudder? Or stall it in a thermalling turn? Does failure to drop the nose at stall really mean it can't spin? Ian -- |
#19
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"Ian Johnston" wrote in message news:cCUlhtvFIYkV-pn2-EdKXeK7dL0Wj@localhost... On Fri, 1 Aug 2003 02:00:17 UTC, "Bill Daniels" wrote: : The Marske planform does eliminate the stall/spin as a likely source of : accidents From what was posted here, it stalls fine but as a mushing stall (which is exactly what I get in a K8). Just as a matter of interest, what happens in a Marske if you stall it and then kick in a bootful of rudder? Or stall it in a thermalling turn? Does failure to drop the nose at stall really mean it can't spin? Ian Ian, Flying both the Pioneer 1A and the Pioneer II, I have held full rudder through a series of stall attempts and all I got was a mushing turn. I was never able to get anything even remotely resembling a spin departure. In several tests I made extreme attempts to get a departure without success. The slow flight behavior is benign in the extreme even with the CG aft of the rear limit. Now, lets talk about stalls. If you get a nose drop, that doesn't necessarily mean a stall has occurred. To my way of thinking, a stall require a substantial disruption of airflow over the upper surface of the wing resulting in loss of lift and a departure from controlled flight. My experience with Marske gliders is the same as other pilots in that the ailerons remain fully effective and the elevator control retains a solid feel. In short, the glider never departs controlled flight. What you do get is a sharp loss of up elevator authority as the AOA exceeds a certain value and the nose bobs down a bit. I really don't feel comfortable calling that a stall since the airflow over the majority (probably the forward 60% of the chord) of the wing remained attached. Even the description, "mushing stall" seems inappropriate. The glider doesn't even sink rapidly at minimum airspeed with the stick full back - it just glides slowly along with all controls fully effective. This doesn't mean you can't crash the glider - it just means you have to work a lot harder to do it. Bill Daniels |
#20
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On Sat, 2 Aug 2003 12:49:49 UTC, "Bill Daniels"
wrote: : My experience with Marske gliders is the same as other pilots in that the : ailerons remain fully effective and the elevator control retains a solid : feel. Sounds just like a mushing stall in a Ka8! : Even the description, "mushing stall" seems inappropriate. The glider : doesn't even sink rapidly at minimum airspeed with the stick full back - it : just glides slowly along with all controls fully effective. Sounds just like a Ka8 with an elevator stop. Primary gliders used to have these ... Ian -- |
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