![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#10
|
|||
|
|||
![]()
At 08:57 10 June 2008, Matt Herron Jr. wrote:
Umm... What happened to the wind tunnel testing that was underway over four years ago? This is where experimentation that requires such tight control of parameters and is so sensitive to humidity, turbulence, etc. should be conducted. If this research looked so promising and was funded by NASA, they have rather lovely tunnels you could put the whole Cirrus into if you wished. I would think that performance questions could be answered in a matter of a month or two. What went wrong there? I am the first to consider that new breakthroughs are almost always met with significant criticism, so I like to fall back on the facts whenever possible. As a sanity check, lets look at the latest comparison flight between the Cirrus @ the claimed 33.5:1 glide ratio and the Dana 1 at 45:1 On one leg that was graphed, the flight lasted 8 minutes with the two aircraft flying side by side at about 51 knots. It looks like the Cirrus kept up quite nicely with the Dana! But lets take a closer look. At 51 knots, that's about 5164 ft/minute forward, and for the Dana, about 114 ft/minute sink in still air. Over the course of the 8 minutes, the Dana should sink 918 ft, and the Cirrus, 1233 ft, so the expected difference in altitude is about 315 ft after 8 minutes of flying. From the trace, both aircraft only sink about 100 feet over this time, and are flying through sink and lift the whole time of strengths up to 4 knots. So one could say that the variation in altitude contributed by the still air sink rate of the gliders is only about 25% of the total. The other 75% is due to flying through rising and sinking air. Given that the gliders were flying side by side through slightly different air, is it possible that any performance variations (good or bad) were completely masked by minor variances in this more dominant variable of moving air masses? It would take an average difference of only 0.37 knots of lift/sink over the flight to account for this. I would like to think it's all true, but so far have little basis other than hope. Get back in the wind tunnel, or show me a 40 minute final glide at 7:am in still air. Matt Matt, Notice how the two aircraft match each other bounce for bounce in both flight legs, especially on the-upwind, cloud-street run. This shows that the aircraft were close enough to be seeing essentially the same air. In fact, we did another, shorter out and return but I did not post that one, because it was clear that the Diana was not matching my "bumps." In fact it lost altitude to my glider, but it was clear that the Diana was too far away. Both flight logs are on the web for you to download. Evidently you looked at them. But I would just like to make the point to everyone that I am not making claims here, I am throwing data at you to deal with. It is what it is! Thank you, Mark, for making an honest effort to deal with the facts. JEH |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
SZD-56-2 Diana | Yurek | Soaring | 23 | September 4th 08 07:31 PM |
SZD-56 Diana | Wayne Paul | Aviation Photos | 0 | March 11th 08 01:19 PM |
Diana-2 VH-VHZ | BlueCumulus[_2_] | Soaring | 3 | July 25th 07 08:00 AM |
SZD-56-2 Diana | Yurek | Soaring | 14 | February 18th 05 01:25 AM |
SZD-56-2 Diana | Yurek | Soaring | 1 | January 29th 05 01:02 PM |