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The "eta and xsi" convention for control surfaces is confusing. Can you please say as to what will the values for eta and psi for a simple flap control surface for a single -wing configuration?
The text was updated successfully, but these errors were encountered:
The "eta and xsi" convention for control surfaces is confusing. Can you please say as to what will the values for eta and psi for a simple flap control surface for a single -wing configuration?
The text was updated successfully, but these errors were encountered: