A commercial aircraft (with a mass of 71411 kg, wing surface area of 119 m² and wing aspect ratio of 10) produces a maximum of 209459 newtons of thrust. Assuming CLMAX = 2.1 and CD Calculate the Climb Rate (in feet/min) at an initial climb airspeed of 169 knots. -89 O 11.79 3570.55 171697.81 2320.13 = 0.06,
A commercial aircraft (with a mass of 71411 kg, wing surface area of 119 m² and wing aspect ratio of 10) produces a maximum of 209459 newtons of thrust. Assuming CLMAX = 2.1 and CD Calculate the Climb Rate (in feet/min) at an initial climb airspeed of 169 knots. -89 O 11.79 3570.55 171697.81 2320.13 = 0.06,
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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