@inproceedings{waithe2008,
	address = {Reno, NV},
	title = {Application of {USM3D} for sonic boom prediction by utilizing a hybrid procedure},
	isbn = {978-1-56347-937-3},
	url = {https://arc.aiaa.org/doi/abs/10.2514/6.2008-129},
	doi = {10.2514/6.2008-129},
	abstract = {The application of USM3D, an unstructured flow solver, to predict sonic boom by using a hybrid computational fluid dynamics procedure on four configurations is presented. The first configuration is a generic wing-body-vertical. The second and third configurations are the Quiet Spike™, which is patented by Gulfstream, attached to equivalent area distributions. The fourth configuration is NASA's F15 with the Quiet Spike attached. Computations on the wing-body-vertical are compared to computational data from a structured flow solver. Computations on the Quiet Spike are compared to wind tunnel tests conducted at NASA Langley Research Center and computational data from a structured flow solver. Computations on the F-15 with the Quiet Spike are compared to flight test data obtained at NASA Dryden Flight Research Center. Results indicate that USM3D is a capable code to be used in a hybrid procedure for predicting sonic boom. Copyright © 2008 by Gulfstream Aeropace Corporation.},
	publisher = {AIAA Paper 2008-129},
	author = {Waithe, Kenrick A.},
	year = {2008},
}

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