Formula Used:
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Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air. It represents the undisturbed flow velocity in fluid dynamics.
The calculator uses the formula:
Where:
Explanation: This formula calculates the freestream velocity based on doublet strength, radial coordinate, radial velocity, and polar angle in a flow field.
Details: Calculating freestream velocity is crucial in aerodynamics and fluid dynamics for analyzing flow patterns around objects, designing aerodynamic surfaces, and understanding potential flow theory applications.
Tips: Enter doublet strength in m³/s, radial coordinate in meters, radial velocity in m/s, and polar angle in radians. Ensure radial coordinate > 0 and polar angle is within valid range (-π/2 < θ < π/2).
Q1: What is doublet strength in fluid dynamics?
A: Doublet strength is defined as the product of the distance between a source-sink pair and source or sink strength, representing the strength of a doublet in potential flow theory.
Q2: Why is the polar angle important in this calculation?
A: The polar angle determines the direction component of the radial velocity relative to the freestream direction, affecting the velocity decomposition.
Q3: What are typical values for doublet strength?
A: Doublet strength values vary widely depending on the specific flow configuration, but are typically positive values measured in cubic meters per second.
Q4: When is this formula applicable?
A: This formula is derived from potential flow theory and is applicable for incompressible, irrotational flow around doublet configurations.
Q5: What are the limitations of this calculation?
A: This calculation assumes ideal potential flow conditions and may not account for viscous effects, compressibility, or real fluid behavior in practical applications.