Abstract
The transonic equivalence rule with lift is studied computationally using the full-potential code. Two pairs of equivalent wings are designed according to the assumptions of the equivalence rule at freestream Mach number = 0.94. One pair of equivalent wings has a concorde-like planform and the other pair has a delta planform with sine tip-fairing. The computed pressure distributions in the outer e owe eld of the two pairs of equivalent wings and the wave drag coefe cients of the former pair are analyzed, and the equivalence rule is verie ed.
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