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  2. Banked turn - Wikipedia

    en.wikipedia.org/wiki/Banked_turn

    This formula also shows that the radius of turn decreases with the angle of bank. With a higher angle of bank the radius of turn is smaller, and with a lower angle of bank the radius is greater. In a banked turn at constant altitude, the load factor is equal to 1 cos ⁡ θ {\displaystyle {\frac {1}{\cos \theta }}} .

  3. Standard rate turn - Wikipedia

    en.wikipedia.org/wiki/Standard_rate_turn

    For aircraft holding purposes, the International Civil Aviation Organization (ICAO) mandates that all turns should be made, "at a bank angle of 25° or at a rate of 3° per second, whichever requires the lesser bank." [4] By the above formula, a rate-one turn at a TAS greater than 180 knots would require a bank angle of more than 25 ...

  4. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    Flight path angle γ: is the angle between horizontal and the velocity vector, which describes whether the aircraft is climbing or descending. Bank angle μ: represents a rotation of the lift force around the velocity vector, which may indicate whether the airplane is turning.

  5. Flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Flight_dynamics

    The equilibrium roll angle is known as wings level or zero bank angle, equivalent to a level heeling angle on a ship. Yaw is known as "heading". A fixed-wing aircraft increases or decreases the lift generated by the wings when it pitches nose up or down by increasing or decreasing the angle of attack (AOA). The roll angle is also known as bank ...

  6. Load factor (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Load_factor_(aeronautics)

    For example, in a turn with a 60° angle of bank the load factor is +2. Again, if the same turn is performed with the aircraft inverted, the load factor becomes −2. In general, in a balanced turn in which the angle of bank is θ, the load factor n is related to the cosine of θ as [1] [2]: 407 = ⁡.

  7. Spacecraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_flight_dynamics

    A space vehicle's flight is determined by application of Newton's second law of motion: =, where F is the vector sum of all forces exerted on the vehicle, m is its current mass, and a is the acceleration vector, the instantaneous rate of change of velocity (v), which in turn is the instantaneous rate of change of displacement.

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  9. Aircraft compass turns - Wikipedia

    en.wikipedia.org/wiki/Aircraft_compass_turns

    This guideline is based not on a standard-rate turn, but on a bank angle of 15°-18°, which would equal a standard rate turn at the airspeeds typical of light aircraft. The pilot community uses the mnemonic UNOS (undershoot North overshoot South) to memorize this rule in the Northern hemisphere. In the Southern hemisphere the mnemonic ONUS is ...