NASA NTRS · 19780010123
Integrated gas turbine engine-nacelle
Abstract
A nacelle for use with a gas turbine engine is presented. An integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine, provides lightweight support. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus while the outer surface of the nacelle defines a streamlined envelope for the engine.
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Adamson, A. P., Sargisson, D. F., Stotler, C. L., Jr.. 1977-10-25. Integrated gas turbine engine-nacelle. https://ntrs.nasa.gov/citations/19780010123
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