in plan having d of 1.8 m. In km/h the total
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
![Q.27. A wing of small aeroplane is
rectangular in plan having a span of 12
m and chord of 1.8 m. In a horizontal
flight at 200 km/h the total aerodynamic
force acting on the wing is 28 kN. If lift-
drag ratio is 10. Determine:
(i) Coefficient of lift and Drag
(ii) Total weight the aeroplane can
carry
(iii) Power required for the flight
= 1.2 kg/m³.
Take Pair](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fd7416c83-8943-48af-9d52-4f0be02a0c0c%2Fb8aa0a9a-d7d0-47e9-96bb-959607352d17%2F2bep7u_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Q.27. A wing of small aeroplane is
rectangular in plan having a span of 12
m and chord of 1.8 m. In a horizontal
flight at 200 km/h the total aerodynamic
force acting on the wing is 28 kN. If lift-
drag ratio is 10. Determine:
(i) Coefficient of lift and Drag
(ii) Total weight the aeroplane can
carry
(iii) Power required for the flight
= 1.2 kg/m³.
Take Pair
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