Theory of FlightA- Airbus 320 fly in steady level flight with altitude 11000m, find the lift forcerequired to steady level flight. At steady level flight aircraft has weight as (65000kg), wing area is (124 m?), aircraft speed is (147 m/s) and lift coefficient is (1.3)Atmosphere data for 11000m shown in table belowТуре ofatmosphere layerStratosphereRang (m) Temperature gradient (a) k/mTemperature (k)0-11000-0.0065288-216.6Given data (R=287, g=9.81 m/s?, and po=1.225 kg/m³)

For the steady level of flight, the lift force is equal to the weight force then the plane is in…

_A- Airbus 320 fly in steady level flight with altitude 11000m, find the lift force required to steady level flight. At steady level flight aircraft has weight as (65000 kg), wing area is (124 m²), aircraft speed is (147 m/s) and lift coefficient is (1.3) Atmosphere data for 11000m shown in table below

_A- Airbus 320 fly in steady level flight with altitude 11000m, find the lift force required to steady level flight. At steady level flight aircraft has weight as (65000 kg), wing area is (124 m²), aircraft speed is (147 m/s) and lift coefficient is (1.3) Atmosphere data for 11000m shown in table below

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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