I am trying to learn about Density Altitude and in doing so I’ve confused myself. I understand DA= Pressure Altitude +[120x(OAT TEMP-ISA TEMP)]
If there’s an easier/friendlier equation I would appreciate it! Anyways
For example
Using a PA (Pressure Alt) of 2150
The only ISA temp rule of thumb I know is
“Double the altitude, subtract 15 and put a - sign on it” -Nicholas Irving Precision Rifle Bible is where I got that “ROT”
In the book as an example for an ISA TEMP at 10,000Ft multiply by 2 to get 20; then subtract 15 to get 5 and add the -. so DA=5470 + [120 x (35-5)] in this example the DA=9,070
My issue is trying to equate this at a pressure alt of 2150ft with a OAT TEMP of 11° C
So I would assume 2150 x 2 = 4300 so I take 43? - 15 which gives me 28 add the - so -28 in an equation of 2150 + [120 x 11 -28)]. 11-28= -17 x 120 = -2040
-2040+2150= 110 so by my math my density altitude is 110ft which I know cannot be correct if I’m at an actual altitude of 1680ft. Because standard pressure is (29.92) SP* and Current Pressure CP* is at 29.45 to get my Pressure Altitude or PA* I take my standard pressure minus current pressure x 1000 + field elevation of 1680 = 2150.
Where am I going wrong?
If there’s an easier/friendlier equation I would appreciate it! Anyways
For example
Using a PA (Pressure Alt) of 2150
The only ISA temp rule of thumb I know is
“Double the altitude, subtract 15 and put a - sign on it” -Nicholas Irving Precision Rifle Bible is where I got that “ROT”
In the book as an example for an ISA TEMP at 10,000Ft multiply by 2 to get 20; then subtract 15 to get 5 and add the -. so DA=5470 + [120 x (35-5)] in this example the DA=9,070
My issue is trying to equate this at a pressure alt of 2150ft with a OAT TEMP of 11° C
So I would assume 2150 x 2 = 4300 so I take 43? - 15 which gives me 28 add the - so -28 in an equation of 2150 + [120 x 11 -28)]. 11-28= -17 x 120 = -2040
-2040+2150= 110 so by my math my density altitude is 110ft which I know cannot be correct if I’m at an actual altitude of 1680ft. Because standard pressure is (29.92) SP* and Current Pressure CP* is at 29.45 to get my Pressure Altitude or PA* I take my standard pressure minus current pressure x 1000 + field elevation of 1680 = 2150.
Where am I going wrong?