The absolute ceiling of an aircraft is the maximum altitude it can reach while maintaining level flight under standard atmospheric conditions, where the rate of climb becomes zero. The formula for calculating the absolute ceiling (habs​) of an aircraft is: Where: T is the thrust produced by the aircraft’s engines, D is the total drag […]
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The rate of ascent of an aircraft refers to the speed at which it climbs vertically in altitude over a given period of time.When an aircraft’s rate of ascent is positive, it means it is ascending; when it is negative, it means it is descending. The formula for the rate of ascent of an aircraft can
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The speed at which an aircraft descends vertically in altitude over a predetermined period of time is referred to as the rate of descent. Numerous factors, such as the aircraft’s configuration, angle of attack, thrust setting, and atmospheric conditions, affect the rate of descent. When an aircraft descends vertically to a lower altitude, the rate
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Thrust vectoring Calculator is a technique used in aircraft and rocket engines to manipulate the direction of thrust. The formula for calculating the effect of thrust vectoring depends on various factors such as the angle of deflection, engine thrust, and the distance between the engine’s center of thrust and the aircraft’s center of gravity. One
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The load factor (n) in a coordinated turn refers to the ratio of the total lift force acting on an aircraft to its weight. It quantifies the additional force experienced by the aircraft due to centrifugal acceleration during the turn. During a coordinated turn, the load factor increases as the bank angle of the turn
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Thrust Augmentation Calculator typically refers to methods or systems used to increase the thrust produced by an engine or propulsion system beyond its normal operating conditions. This can involve various techniques such as afterburners in jet engines, water injection in piston engines, or adding external boosters to rocket engines. Thrust Augmentation Calculator, a pivotal concept
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The bank angle is the angle between the aircraft’s longitudinal axis and the horizontal plane. It determines the rate at which the aircraft changes its heading during a turn. A bank angle results in a tighter turn, while a shallower bank angle results in a gentler turn. The formula to calculate the bank angle as
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The kinetic energy KE of an object is defined as the energy it possesses due to its motion. It can be calculated using the formula Where: m is the mass of the object (in kilograms, kg), v is the velocity of the object (in meters per second, m/s).
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The flexural stress calculator determines the stress experienced by a material subjected to bending, also known as bending stress, using the given formula. M is the bending moment applied to the beam. c is the distance from the neutral axis to the outermost fiber (also known as the distance to the centroid). I is the
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Column Buckling Calculator is a sudden deformation of vertical support under compressive load. The formula is given by: Where: Pcr​ is the critical buckling load, E is the modulus of elasticity of the column material, I is the area moment of inertia of the column’s cross-sectional shape, Leff​ is the effective length of the
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