LIFT to drag ratio is USED to provide information about aerodynamics of the AIRCRAFT. It is often termed as aerodynamic efficiency. Thrust to WEIGHT ratio is called Thrust loading.

"> LIFT to drag ratio is USED to provide information about aerodynamics of the AIRCRAFT. It is often termed as aerodynamic efficiency. Thrust to WEIGHT ratio is called Thrust loading.

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Damping ratio is defined as __________

Aircraft Design Dynamic Stability in Aircraft Design . 3 years ago

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Damping ratio is defined as ratio of damping coefficient to the critical damping coefficient. LIFT to drag ratio is USED to provide information about aerodynamics of the AIRCRAFT. It is often termed as aerodynamic efficiency. Thrust to WEIGHT ratio is called Thrust loading.

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Posted on 30 Mar 2022, this text provides information on Aircraft Design related to Dynamic Stability in Aircraft Design. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.

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