Q4. Light weight airplane (11000 N), propeller disc diameter (1.6 m), wing area is (30.6 m2) and airplane drag polar (CD=0.034+0.0544 CL') flight altitude is (2000 m) velocity (190 Km/hr.) Calculate the velocity of slip stream far behind the propeller and the ideal efficiency of the propeller? (20 degree)
Q4. Light weight airplane (11000 N), propeller disc diameter (1.6 m), wing area is (30.6 m2) and airplane drag polar (CD=0.034+0.0544 CL') flight altitude is (2000 m) velocity (190 Km/hr.) Calculate the velocity of slip stream far behind the propeller and the ideal efficiency of the propeller? (20 degree)
Related questions
Question
I need the answer as soon as possible
Transcribed Image Text:Q4. Light weight airplane (11000 N), propeller disc diameter (1.6 m), wing area is
(30.6 m2) and airplane drag polar (CD=0.034+0.0544 CL') flight altitude is (2000
m) velocity (190 Km/hr.) Calculate the velocity of slip stream far behind the
propeller and the ideal efficiency of the propeller? (20 degree)
Expert Solution
This question has been solved!
Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.
Step by step
Solved in 2 steps with 2 images
