Holy moly! Mytho-GR1 passing the test called “basic reading comprehension”!
I know i know it is a hard skill nowadays
By definition and by design flaps affect lift.
14 degrees AOA results in 6G at 390 knots
What does 14 degrees AOA result in in your chart at 390
Not really for this
If by his chart you mean the AV-8A manual, then near enough exactly 5g.
Removing 1/2 a ton of weight from the aircraft will indeed have effects on the turn performance. This should be readily obvious to anyone with two functioning braincells.
Do you understand physics
Do you?
Yes
well you clearly dont given
that is such an absurd statement
like why would you add flaps if they dont affect lift, them affecting lift is the entire reason they have been developed and added to aircraft
I have compounding data for no flaps as well.
According to the actual ODM manual the harrier 1 with no flaps will produce 89,000lbs lift at 400 knots in buffet.
This is 11-12 degrees AOA.
At 17,200 lbs that is how many G, let’s see if you can math (it’s 5.2G ish)
What does your chart say for no flaps 12 degrees AOA at 400 knots for the same weight???
4.1 ish
Now tell me why is it different by an entire G.
Ahh wait the harrier is underperforming in lift when compared to all other data.
wow, you even posted a source showing that the flaps affect lift
No I showed a source showing that flaps alter the usable buffet limits as they encourage the airflow and delay the onset of buffet.
I’m getting to my point so chill
yep, you dont at all know what you are talking about
Read what I said above
yeah, and it shows you dont know what you are talking about
no reason to keep arguing with you at this point with how uninformed you are
Maybe you can’t read not my problem I haven’t been arguing with you in the first place.
The ODM manual gives an entire G more at the gate gen AOA for the given weight and flap setting.
Lmfao
You realize that’s just the denotation for the 14-16-18 lines right? X by 1000 to get the weight…