Repeat Example 5 .4 using the SDPM and compare the resulting pressure distributions to the experimental pressures
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Repeat Example 5 .4 using the SDPM and compare the resulting pressure distributions to the experimental pressures given in Kolbe and Boltz (1951).
Data from Example 5.4
Use the VLM to calculate the aerodynamic loads acting on a swept wing at several angles of attack and compare to experimental data.
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Related Book For
Unsteady Aerodynamics Potential And Vortex Methods
ISBN: 9781119762539
1st Edition
Authors: Grigorios Dimitriadis
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