Difficulty: Easy
Correct Answer: True
Explanation:
Introduction / Context:
In fluid mechanics and aerodynamics, forces on immersed bodies are resolved into components. Two standard components are drag (along the free stream) and lift (perpendicular to the free stream). A flat or curved plate placed at an angle to the oncoming flow experiences a pressure and shear distribution that results in a net force with these two components.
Given Data / Assumptions:
Concept / Approach:
By definition, the component of the resultant fluid force perpendicular to the undisturbed flow direction is called lift. The component parallel to the undisturbed flow direction is called drag. This definition applies broadly, regardless of whether the plate is a wing, hydrofoil, or a simple immersed flat plate at an angle of attack.
Step-by-Step Solution:
Identify the resultant pressure and shear force on the plate due to the flow.Resolve this resultant into components along and normal to the free stream.Name the along-stream component as drag and the normal component as lift.Hence, the statement given is precisely the definition of lift → it is correct.
Verification / Alternative check:
In wing theory, lift L and drag D are often expressed using coefficients (C_L and C_D) relative to dynamic pressure and planform area. The orientation of these forces is always defined with respect to the free stream, not to the body surface, which confirms the perpendicular component is lift.
Why Other Options Are Wrong:
Common Pitfalls:
Final Answer:
True
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