Difference between revisions of "User talk:Suprā"

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(Created page with "==horsepower graphs== I'm not sure where you are getting those numbers. They are wrong.--~~~~")
 
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==horsepower graphs==
 
==horsepower graphs==
 
I'm not sure where you are getting those numbers. They are wrong.--[[User:U30585107|U30585107]] ([[User talk:U30585107|talk]]) 01:17, 8 November 2019 (UTC)
 
I'm not sure where you are getting those numbers. They are wrong.--[[User:U30585107|U30585107]] ([[User talk:U30585107|talk]]) 01:17, 8 November 2019 (UTC)
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:The expected values for the F-82e's WEP horsepower for 1 engine based on the code are
 +
{| class="wikitable"
 +
|-
 +
! Alt !! WEP HP
 +
|-
 +
| 0 m || 1955
 +
|-
 +
| 1000 m|| 1955
 +
|-
 +
| 6095 m || 1700
 +
|-
 +
| 9143 m || 1329
 +
|}
 +
:with a straight line connecting the points. So your graph is shaped correctly aside from the beginning values. Judging by my rough eyeballing of of your horsepower values your numbers are a bit off. Could you show me your raw data? Also please do not test in the test flight map many people have claimed it is inaccurate.--[[User:U30585107|U30585107]] ([[User talk:U30585107|talk]]) 02:45, 9 November 2019 (UTC)
 +
::The 1955 might look odd then you'll be even more surprising that the 100% hp of the F-82 is 1600hp from 0 m all the way to 6095m. Feel free to test it.
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::I'm not sure what would be the best map but I see there is a variance in atmospheric pressure between maps. Perhaps a map with as close to 1 atm at sea level would be optimal? I think some of the deviation from the expected values might also be from the speed of the plane. I tested the plane at ~300km/h and 1000m and got ~1800hp while going at ~640km/h got ~1930hp. I know jets exhibit this behavior but I've never seen it documented for prop planes as well.--[[User:U30585107|U30585107]] ([[User talk:U30585107|talk]]) 05:21, 9 November 2019 (UTC)
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:::If it does follow the same behavior as jets then it should have a U shaped curve where you get the maximum horsepower at 0 speed. Why it works that way, I don't know.--[[User:U30585107|U30585107]] ([[User talk:U30585107|talk]]) 01:56, 10 November 2019 (UTC)

Revision as of 01:56, 10 November 2019

horsepower graphs

I'm not sure where you are getting those numbers. They are wrong.--blastedryan (talk) 01:17, 8 November 2019 (UTC)

The expected values for the F-82e's WEP horsepower for 1 engine based on the code are
Alt WEP HP
0 m 1955
1000 m 1955
6095 m 1700
9143 m 1329
with a straight line connecting the points. So your graph is shaped correctly aside from the beginning values. Judging by my rough eyeballing of of your horsepower values your numbers are a bit off. Could you show me your raw data? Also please do not test in the test flight map many people have claimed it is inaccurate.--blastedryan (talk) 02:45, 9 November 2019 (UTC)
The 1955 might look odd then you'll be even more surprising that the 100% hp of the F-82 is 1600hp from 0 m all the way to 6095m. Feel free to test it.
I'm not sure what would be the best map but I see there is a variance in atmospheric pressure between maps. Perhaps a map with as close to 1 atm at sea level would be optimal? I think some of the deviation from the expected values might also be from the speed of the plane. I tested the plane at ~300km/h and 1000m and got ~1800hp while going at ~640km/h got ~1930hp. I know jets exhibit this behavior but I've never seen it documented for prop planes as well.--blastedryan (talk) 05:21, 9 November 2019 (UTC)
If it does follow the same behavior as jets then it should have a U shaped curve where you get the maximum horsepower at 0 speed. Why it works that way, I don't know.--blastedryan (talk) 01:56, 10 November 2019 (UTC)