Supersonic aircraft with spike for controlling and reducing sonic boom

1. Field of the Invention An aircraft includes a spike projecting forward from the leading end of the fuselage and/or rearward from the trailing end of the fuselage. The spike can include a single section or two or more sections of varying cross-sectional area. Transition regions between sections of...

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Bibliographische Detailangaben
Hauptverfasser: Henne, Preston A, Howe, Donald C, Wolz, Robert R, Hancock, Jr., Jimmy L
Format: Patent
Sprache:eng
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