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