1977•Unpublished venueRequires access

Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78. [conducted in the Lewis 8 by 6 foot tunnel

O. D. Wells, Michael López, H. Robert Welge, P. A. Henne, A. E. Sewell

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Key concepts: Mach number, Propulsion, Aerospace engineering, Aeronautics, Wing, Wind tunnel, Engineering, Environmental science

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Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78. [conducted in the Lewis 8 by 6 foot tunnel — Research Paper | ScholarLens