Repeat Example 6 .5 for the pitching oscillation test case at k = 0 .262 and M
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Repeat Example 6 .5 for the pitching oscillation test case at k = 0 .262 and M∞ = 0 .498 reported in Zwaan (1982). How good is the agreement between the SDPM and experimental oscillatory pressures? Does the agreement improve if you increase the number of spanwise panels to, say, n = 40 ?
Data from Example 6.5
Use the SDPM in order to predict the unsteady pressure distribution around a NLR 7301 airfoil with an oscillating flap.
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Related Book For
Unsteady Aerodynamics Potential And Vortex Methods
ISBN: 9781119762539
1st Edition
Authors: Grigorios Dimitriadis
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