Repeat Example 5 .10 for the other two wings tested by Queijo et al. (1956) and compare
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Repeat Example 5 .10 for the other two wings tested by Queijo et al. (1956) and compare the VLM predictions to the experimental measurements.
Data from Example 5.10
Calculate the roll stability derivatives for a flat-plate wing with aspect ratio 6 and taper ratio 0.6 and compare to experimental measurements.
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Related Book For
Unsteady Aerodynamics Potential And Vortex Methods
ISBN: 9781119762539
1st Edition
Authors: Grigorios Dimitriadis
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