1954•Unpublished venueRequires access

The Effect of an Operating Propeller on the Aerodynamic Characteristics at High Subsonic Speeds of a Model of a Vertical-rising Airplane Having an Unswept Wing of Aspect Ratio 3

Fred B Sutton, Donald A Buell

Abstract

Report presenting an investigation in the pressure wind tunnel to determine the effect of an operating propeller on the aerodynamic characteristics of a model of a vertical-rising airplane with an unswept wing with an aspect ratio of 3. Lift, longitudinal force, pitch, and roll characteristics, with and without power, are presented for the complete model and various combinations of model components.

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Key concepts: Airplane, Aerodynamics, Wing, Propeller, Lift (data mining), Wind tunnel, Engineering, Marine engineering