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Posted

Just wanted to start a discussion on people’s thoughts and observations on the flight model. 
One thing that immediately jumped out to me during my testing is the proverse yaw. In low to medium AoAs the aircraft has a pretty strong proverse yaw response. Which I found a bit surprising, considering the MiG 29 uses spoilers and a bit of differential stabilizer to roll the aircraft. I read in the real world manual about the spoilers being up 5 degrees from neutral to help reduce adverse yaw, but nothing about eliminating it or proverse yaw. I’m not saying this is unrealistic, as I don’t know, just that I would think the aircraft would have adverse yaw instead of proverse. 
Anyone out there that perhaps knows any real MiG drivers that can ask if this is indeed accurate? Or if someone has a manual that describes this characteristic?

I saw GVad the Pilots YouTube video about the flight model. Seems to be slightly underperforming in high speed flight as well?

All in all it does feel great to fly! Doing tail slides is fun and it seems to behave just like how you see in real videos from airshows 

Posted

You're probably talking about the before-1 patch video, here's the after video, it looks pretty good:

 

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Posted

The only thing I notice it’s turning behavior. According to charts it should hit sustained 9 G right at 900 kmh, and maintain max G until supersonic speed. Right now it stops maintaining 9 G will before supersonic speed

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Posted
1 hour ago, AeriaGloria said:

The only thing I notice it’s turning behavior. According to charts it should hit sustained 9 G right at 900 kmh, and maintain max G until supersonic speed. Right now it stops maintaining 9 G will before supersonic speed

Sadly, this is a very vague comment; without knowing drag index, gross weight, altitude, and throttle setting, we really can't say if there is an issue or now, as well as what charts you are referencing, etc. 

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Posted (edited)
1 hour ago, NineLine said:

Sadly, this is a very vague comment; without knowing drag index, gross weight, altitude, and throttle setting, we really can't say if there is an issue or now, as well as what charts you are referencing, etc. 

I am referencing German TO-1 that can be purchased from Amazon and also appears in the L-18 manual which can also be purchased on Amazon, and most importantly the instantaneous G chart from the same German TO-1 that can be purchased on Amazon. As well as many comments in practical aerodynamics saying it is not until you hit Mach 1 that the elevator loses efficiency and stops you from pulling max G. This sustained turn chart shows both drag and gross weight and so should be able to atleast hit those numbers. The instantaneous G chart doesn’t say exactly drag and weight just “clean or with missiles”, but if it’s like every other single chart it is for 2x R-73, 4x pylons, and 13,000 kg weight with approximately 1,500 kg fuel. Either way it should hit these numbers at some point in the flight envelope. The creators of the chart clearly thought it correct enough for a wide enough range to say “clean or with missile load CG 25.5%”
 

Notice how at low altitudes it has no  problem hitting max G until is just past Mach 1. This is also the exact reason the ARU system is tuned to start giving authority back at 1200 kmh. 

 

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Edited by AeriaGloria

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