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 HomeGATEAn 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 15gate questionsQ. 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 isAns: 62.00 to 63.50
Some students were not involved in the strike. If the above statement is true, which of the following conclusions
The radius as well as the height of a circular cone increases by 10%. The percentage increase in its volume is
