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Wind tunnel investigation of airframe installation effects on underwing engine nacelles at Mach numbers from 0.56 to 1.46

B. J. Blaha, D. C. Mikkelson

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Abstract

Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing engine nacelles at Mach 0.56 to 1.46

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Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing engine nacelles at Mach 0.56 to 1.46

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OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing engine nacelles at Mach 0.56 to 1.46

Key concepts: Nacelle, Airframe, Mach number, Wind tunnel, Supersonic wind tunnel, Aeronautics, Aerospace engineering, Engineering

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Wind tunnel investigation of airframe installation effects on underwing engine nacelles at Mach numbers from 0.56 to 1.46 — Research Paper | ScholarLens