Repeat Example 5 .13 for all Mach numbers tested by Lessing et al. (1960) using the incompressible

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Repeat Example 5 .13 for all Mach numbers tested by Lessing et al. (1960) using the incompressible SDPM code of the same example. How bad do the incompressible predictions get at Mach numbers of 0 .7 and 0 .9?

Data from Example 5.13

Use the frequency domain version of the SDPM to calculate the unsteady pressure distribution on a wing oscillating in the first bending mode.

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Unsteady Aerodynamics Potential And Vortex Methods

ISBN: 9781119762539

1st Edition

Authors: Grigorios Dimitriadis

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Question Posted: May 03, 2024 04:00 AM

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Repeat Example 5 .13 for all Mach numbers tested by Lessing et al. (1960) using the incompressible

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Unsteady Aerodynamics Potential And Vortex Methods

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