If my aircraft has access power off 520 KW and it weighs around 1200 N then, determine the value of specific excess power.
(a) 433.33 m/s
(b) 123.88 ft. s
(c) 119
(d) 345.768m/s
The question was asked in final exam.
Question is from Flight Mechanics in section Performance and Flight Mechanics of Aircraft Design