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6

The MiG-29 series of aircraft are designed to operate from poor quality airfields, and for this reason, they feature separate air intakes for use while moving on the ground. See this article, including pictures of the aircraft: https://www.airforce-technology.com/projects/mig29/ Notice the additional louvre-shaped intakes on top of the aircraft's leading ...


5

The aircraft is equipped with seven (7) integral fuel tanks: five (5) Center body fuel tanks and two (2) wing tanks. Center body fuel tank #2 serves an an engine feeder tank with all other tanks transferring fuel to it via a network of fuel pumps for consistent weight and balance. The aircraft can be refueled by means of a single pressure refueling ...


5

Like every plane, the MiG-29 stores its fuel in fuel tanks ;) On a more serious manner: Generally speaking, there are 6 internal fuel tanks: 4 distributed around the fuselage and 1 in each wing. Later versions (namely the SMT) have larger internal fuel capacity thanks to the enlarged spine. The exact locations of these tanks can be seen in this cutaway (...


5

The pictures in the question show the normal position of the MiG-29 ailerons. That's how they are unless a roll is commanded. According to Mikoyan Mig-29 Fulcrum Pilot's Flight Operating Manual (google books) the slight upward position is set to improve yaw stability during roll meneuvers: As for whether this angle (neutral position of ailerons) changes in ...


3

@George already gave a correct answer, but I'll expand it a bit and show the source. Indeed, the lower load limit is for trans- and supersonic flight (formally M > 0.85) and the higher limit is for subsonic conditions. The AoA redline at 15° also relates to M > 0.85. At subsonic speeds, the max AoA is 26°. I can only speculate why it is not shown on the ...


2

The line that is at the 9 G's is limit of maximum amount of G's( 9) until 0.85Mach (that is subsonic speed) and the lower line@7.5 is the limit for supersonic flight.


1

On these modern aircraft, there is a thing called flaperons - meaning ailerons and flaps combined, which both move down and up when more lift is needed (TO, LDG and also during some aggressive maneuvers), and are used in order to roll the aircraft. Also- traditionally- you would assume that the plane uses his tail elevators for pitch, but the contrary is ...


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