Repeat Example 5 .7 using the SDPM. Are the differences in the predictions of the two methods
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Repeat Example 5 .7 using the SDPM. Are the differences in the predictions of the two methods more important for the lift or for the thrust/drag? Do these differences reduce as you reduce the thickness of the airfoil?
Data from Example 5.7
Use the unsteady VLM to estimate the thrust produced by a harmonically plunging and pitching rectangular wing.
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Related Book For
Unsteady Aerodynamics Potential And Vortex Methods
ISBN: 9781119762539
1st Edition
Authors: Grigorios Dimitriadis
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