hassan1
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and last but not the least is it possible if you can post details of all colored birds/display teams used by PAF from Red Dragons till 17 Sqn F-7PG?
The painting of Sabre is not bad but there are some techincal mistakes like the three 0.5 inch (12.7 mm) calibre guns on each side of the fuselage are not in order. The guns are placed in an arrow head type arrangement with the middle gun protuding ahead of the top and bottom gun.
Then it seems that you have placed rocket pods on the wrong pylon. The pylon that you have used is a wet pylon, used for carrying the fuel tank. The inboard underwing pylon was used for rocket pods.
Also you have combined flaps and ailerons, which is wrong in case of F-86. Yes you can add full-span slats on them but not full-span flaps.
Does a plane burnt more gas to sustain lower speed on high attitude ...for example refueling ??
We notice second world war plane had frequent problem of stall....is this common technical issue, can we still find this problem in modern fighters. If it happened what are chances of survival for fighter during air combat ???...
Every Fighter has a limit and after that it will stall. Stall means it runs out of air speed, Even fighters like F-22 with such Weight to Thrust Ratio will stall at a certain point.
In war if you stall either you end up in Hell or Heaven there is no 3rd option.
Nice question
lets start with the basics at low altitude we have more Oxygen more Friction which means more Drag. So at any speed it will suck your tank dry because of the above conditions.
Now when we are at higher altitude we have less Oxygen less Drag so it will not burn more Fuel. If you have noticed that all commercial airlines which are crossing over that Atlantic or any other ocean will be at a higher altitude to cross 5 to 6 thousand miles they climb higher. The longer the trip the higher the altitude.
Sir, what is the post-stall maneauver, and what is its significance when related to thrust vectoring? I watched a Canadian show in which they told Canadian Air Force recruits not go below 180knots in their CF-18s, and if they did, to dive and build up air-speed to 180knots before continuing. Is that the post-stall maneuver?
Sir, what is the post-stall maneauver, and what is its significance when related to thrust vectoring? I watched a Canadian show in which they told Canadian Air Force recruits not go below 180knots in their CF-18s, and if they did, to dive and build up air-speed to 180knots before continuing. Is that the post-stall maneuver?