Aerospace Engineering > GATE 2022 > Aircraft Orientation
For a conventional airplane in straight, level, constant velocity flight condition, which of the following condition(s) is/are possible on Euler angles (φ, θ, ψ), angle of attack (α) and the sideslip angle (β)?
A
φ = 0°, θ = 2°, ψ = 0°, α = 2°, β = 0°
B
φ = 5°, θ = 0°, ψ = 0°, α = 2°, β = 0°
C
φ = 0°, θ = 3°, ψ = 0°, α = 3°, β = 5°
D
φ = 0°, θ = 5°, ψ = 0°, α = 2°, β = 5°

Correct : a

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Related Topics

Euler angles angle of attack sideslip angle straight level flight aerospace engineering GATE 2022 GATE AE 2022 Q45 aircraft flight conditions flight dynamics

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