ATPL Theory - Point of Safe Return (PSR) / Point of Equal Time (PET) Also known as “Critical Point” and “Point of No Return”, these two formulas should be considered when planning
CALCULATION OF POINTS OF NO RETURN (PNR) AND CRITICAL POINTS (CP)
CALCULATION OF POINTS OF NO RETURN (PNR) AND CRITICAL POINTS (CP)
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PDF) Range and Endurance Estimates for Battery-Powered Aircraft
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Range Summary
SOLVED: 10. An aircraft weighs 100 kN, has wing surface area of 50 m? and its maximum coefficient of lift is 2. It is powered by jet engines that produce maximum 12
Range Summary
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Range and Endurance for the electrical-only case. | Download Table
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aerodynamics - How can I calculate the optimum loiter airspeed for an aircraft? - Aviation Stack Exchange
