![]() |
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 |
#21
|
|||
|
|||
![]()
Hi,
ArtP, which version of WingX do you have? I just ran it on the latest 2.0.4.3 and WingX came up with PA=1000' and DA=1931'. Interestingly with a dew point of 18C, WingX shows the DA going up to 2,213', that about a 300' difference not that much - would be interesting to see how it affects the performance numbers though. Keep well, Hilton "ArtP" wrote in message ... On Sun, 29 Apr 2007 17:20:43 GMT, "Dallas" wrote: Here's a sample problem: Field Elevation: 1165 Altimeter Setting: 30.10 Temperatu 21°C ___________________ I entered them on my WingX E6B software on my Axim and got PA=995 and DA=1925 |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Air density question?? Pilot's Handbook ofAeronautical knowledge | karl gruber | Piloting | 9 | June 29th 06 08:28 PM |
VOR disparity | Rich S. | Home Built | 7 | January 4th 06 08:31 PM |
atmospheric density effects on airfoils | Stubby | General Aviation | 5 | June 24th 05 02:43 AM |
Student needs assistance density altitude calcs | hellothere.adelphia.net | Rotorcraft | 4 | August 19th 04 07:25 AM |
Pressure Altitude or Density Altitude | john smith | Piloting | 3 | July 22nd 04 10:48 AM |