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The Harmonic Gradient Method (HGM) developed for nonplanar wings in unsteady supersonic flow is generalized to include asymmetric bodies and wing-body combinations. The H-G model is incorporated with a newly developed Bundled Triplet Method (BTM) for treatment of arbitrary bodies. The present method is an effective one in handling unsteady wing-body interference. In particular, the BTM has proven to be computationally more efficient than the surface panel method
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García-Fogeda et al. (1990) studied this question.
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