The drag force experienced by a commercial transport (such as a 787) in cruise depends on its surface area (A), its velocity (V ), the speed of sound (a), the density (ρ) and viscosity (µ) of the fluid, and its angle of attack (α). (a) Express the non-dimensional drag as a function of the other non-dimensional groups. (b) Tests on a model 787 are performed at 1/40th scale. Assume that the speed of sound in the wind tunnel is one-half the speed of sound of the full-scale aircraft. To achieve dynamic similarity in the model test, what would the wind tunnel speed need to be in the model compared to the full-scale prototype? What would the kinematic viscosity of the wind tunnel fluid be compared to air?

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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The drag force experienced by a commercial transport (such as a 787) in cruise depends on its surface area (A), its velocity (V ), the speed of sound (a), the density (ρ) and viscosity (µ) of the fluid, and its angle of attack (α).

(a) Express the non-dimensional drag as a function of the other non-dimensional groups.

(b) Tests on a model 787 are performed at 1/40th scale. Assume that the speed of sound in the wind tunnel is one-half the speed of sound of the full-scale aircraft. To achieve dynamic similarity in the model test, what would the wind tunnel speed need to be in the model compared to the full-scale prototype? What would the kinematic viscosity of the wind tunnel fluid be compared to air?

 

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