The Mannequin challenge is just a response when their staged game of rescue was caught on the camera and got leaked
They might well say the many other acts of rescue were Mannequin challenge and not real rescue.

It feels like none of you have Internet or Google or YouTube or Facebook or any sort of social media or search engine.
Go on YouTube and search “Mannequin challenge” just watch any of them video, then come back and watch the white helmet video. Then tell me they are not trying to replicate the challenge. Why do you think they have to keep stationary when the camera moving around? if they wanted to fake a battlefield rescue video then there would be no point to do that.And they wouldn’t upload a video like that either. No doubt that this thread is full of members that don’t like American but this is just borderline retarded. So desperate to find an “evidence” that fit your narrative that you ignore common sense.
Yeah, sure. Just another one “peacful and harmless mannequin of the innocent civilian victim of the Bloody Regime”.
For **** sake , why is it so hard for you to open the links and read ?
The man and the White Helmets appear frozen. The whole scene is in fact posed.
The men are performing their version of the Mannequin Challenge in a video released by activists from the Revolutionary Forces of Syria (RFS) “to raise awareness of the suffering of the Syrian people”.
http://www.bbc.co.uk/news/world-middle-east-38066791
Of course the video is staged , everyone know that , even the group which released the video said it is staged to replicate Mannequin Challenge. Do you know what the Mannequin Challenge is ?. No one said the video is recorded in real battlefield. If they wanted to fake a recuse in battle field , there wouldnt be the part where the camera moving and the people are stationary. And there wouldn’t be the part where they pose together for a selfie. Seriously , how retarded are people to believe that video is an evidence of white helmet staged their rescure victims ?
My point was if there was either a Wedgetail E-7A, as an airborne command centre it would have a full view of the attack and what was happening; or, if there was a Reaper (UK or otherwise), it would also have had a bird’s eye view of what was happening in the attack which it would be live streaming on a video link and that the attackers would have known it was Syrian Government troops on the heights they were attacking (and where the Syrians had been for years), while the ISIS/”moderate” terrorist forces concentrated and waiting to attack below would also have been picked up over the duration of the attack (about an hour).
If only identify friend and foe could be that simple , we would never have friendly fire. But target on screen look more like this

There was even an incident that an AH-64 friendly fire on their own troop. And that thing has FLIR
The so-called “White Helmets” is a front organisation (not connected to the official government Civil Defence) and who been carrying out fake and staged “rescues”
They are funded to the tune of millions of dollars by terror and ISIS sponsors Qatar, the US and other EU (including rich individuals and other governments trying to take down Assad).
I havenot look at the rest of your post but this video is just ******* stupid.
The specific video you uploaded is one of their Mannequin challengevideo to raise awareness, it cannot be used as an evidence of staged rescues
http://www.dailymail.co.uk/news/article-3975698/Syrian-White-Helmets-rescue-group-upload-Mannequin-Challenge-video.html
Only problem was that Assad was not playing ball and rejected the Qatar and Saudi offer of their pipeline across his country and soon afterwards they set up and paid for the fake “Free Syrian Army”.
When did this happened ?
Stop the BS Levsha, you are ridiculous.
But I’m mildly amused by the fact that you are claiming that the US friendly-fired on their foes 🙂
Nic
More ridiculous is the amount of anti American accusation without proper evidence
knots or IAS.. it doesn’t matter much
knots = 1.852 km/h
IAS = indicated air speed which change dramatically with altitude even if aircraft moving at the same speed
And IAS can either be in knots or mph
In other words , it matter alot
Next stupid thread will perhaps be the F-35 out leg the Flanker or something along those lines..
And why would that be stupid ? the yet have more fuel fraction and quite efficient engine. It entirely possible that it could out range the Flanker
So:
acceleration=climb rate*g/speed.
So at level flight it would be climb rate/speed ? can you do an example ?
That being said, if you calculate acceleration from the climb rate graphs that TsAGI data gives
How to calculate acceleration from climb rate graph? and can we see the graph?
hm, would like to see a JSR vs byoin debate
I would hope that happen so they occupied the others and don’t ruin any other thread
This is wrong. Both are maneuvering conditions. First is for air to air configuration; Clmax = 1,85 and 24 deg maximum AOA. Second is for aircraft with 4000kg or more “aerial bombing ordnance” suspension weight. Its directly comperable to CAT-I and CAT-III limiters on F-16.
For better info: АБСП abberation means = авиационные бомбардировочные средства поражения = aerial bombing ordnance…
Further down the page tells about more limits with different payloads. Also, this graph shows better when those AOAs for both conditions are allowed:
[ATTACH=CONFIG]249901[/ATTACH]
As you can see, first condition (Clmax=1,85) is applicable up to M0,48 at sea level, where it will yield;
0,5*62*1,85*(343,1*0,48)^2 / 9,8184 = 193909 kg of lift. Divide that to 21400 kg as given in the manual its 9Gs.
If we are talking about maneuverability of Su-27 (which I would think it won’t be maneuvering with 8xFAB-500 bombs) its the first graph that matters.
Andraxxus, what do you think about acceleration estimations on first page? reasonable or nah?.
1.85 is when tailing edge flap is fully deployed (level flight only), which could not be used in High G turn
what is tailing edge flaps?
Very clever , now you purposely change my words to make it ridiculous. Nice try but too bad for you no one here is dumb enough to fell for that trickery
Stop responding to JSR, he is a troll with no argument or knowledge. Keep going and his only argument would be “domestic version is different” and “Russian are very technology advanced”
you are embrassing yourself with such simplistic statements
The only one here that should be embarrassed is you
May be adding DI of central pylon too?. One thing that been bugging me though, why the heck HAF manual not have DI for CFT? their F-16 carry that tumor thinggy all the time
According to this http://defense-update.com/products/c/F-16-CFT.htm
“A set of CFTs carries 50 percent more fuel than the centerline external fuel tank, but has only 12 percent of the drag.” The CFTs are designed for the full F-16 flight envelope – up to 9 g’s, maximum angle of attack and sideslip and maximum roll rate.
Centerline tank has drag index of 18 when fully loaded , centerline pylon has drag index of 7
So 12*( 18+7)/100 =3 even less drag than a single Aim-120
All available in manual
^ That true
From flight manual , LAU-118 has drag index of 17 , AGM-88 has drag index of 8. Wing tip missiles has drag index of 0. So with 2 AGM-88 and 2 AIM-120, F-16 will have drag index of 50. With 4 AGM-88 and 2 AIM-120 , F-16 will have drag index of 100
With drag index of 50 and about 50% internal fuel , F-16 max altitude is 53k feet and top speed is Mach 1.9. With drag index of 100 ,F-16 top speed reduced to Mach 1.79
Says another nationalistic troll :angel:
When and how am i a troll ? , are you just mad because i disagree with your Rafale obsession.And if iam a troll then what does that make you ?