At a fixed ground speed, headwind increases airspeed, raising aerodynamic lift and drag. Under the propeller model intended, greater advance speed reduces thrust. The airplane reaches its required take-off airspeed at a lower ground speed, shortening the ground roll. Therefore the assertion that distance increases is false, D.
More Airplane performance: drag polar, take-off and landing, climb and descent, ceilings, range and endurance, load factor, turning flight, V-n diagram, winds questions
GATE 2019 AE Q27– An airplane with maximum lift-to-drag ratio 18 begins an ideal glide at an altitude of 4…
GATE 2019 AE Q51– An airplane weighs 8000 N and has wing area 16 m², zero-lift drag coefficient 0.02, Oswald…
GATE 2019 AE Q53– A propeller airplane initially weighs 4905 N, has wing area 6.84 m² and maximum C L3/2/C…
GATE 2024 AE Q20– Which one of the following figures represents the drag polar of a general aviation…
GATE 2024 AE Q28– Which of the following statements about a general aviation aircraft, while operating at…
GATE 2024 AE Q47– Which of the following statements about absolute ceiling and service ceiling for a…