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Showing 1 to 2 of 2 for “"Propulsion-Airframe Integration"”.

  1. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft

    … varied the nacelle location across a baseline airframe configuration was completed with the Euler solver, and it showed that appreciable overlap between the wing and nacelle led to large increases in interference drag. A follow-on study was conducted with RANS CFD where the wing shape was …

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