A non-VTOL ‑ghter aircraft is climbing vertically at sea level. The aircraft has two turbofan engines; both engines have positive it degrees of setting angle. Draw the side view of the aircraft with an arbitrary angle of attack. Then, derive the governing equations of motion for this climbing ­ight.

A non-VTOL ‑ghter aircraft is climbing vertically at sea level. The aircraft has two turbofan engines; both engines have positive it degrees of setting angle. Draw the side view of the aircraft with an arbitrary angle of attack. Then, derive the governing equations of motion for this climbing ­ight.

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