![An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15](https://www.gkseries.com/blog/wp-content/uploads/2023/09/An-aircraft-with-mass-of-400000-kg-cruises-at-240-m-s-at-an-altitude-of-10-km.-Its-lift-to-drag-ratio-at-cruise-is-15.jpg)
Q. An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is
Q. An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is
Government Schemes Mock Test | Start Test! |
Political Science Mock Test โ 42 | Start Test |
History Test โ 190 | Start Test |
Quantitative Aptitude Test | Start Test! | Data Interpretation - Mock Test | Start Test! |
General Awareness - Mock Test | Start Test! |
Reasoning Ability - Mock Test | Start Test! |