THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWIN-FUSELAGE CONCEPT.

Richard M. Wood, David S. Miller, Kenneth Steven Brentner

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Abstract

A theoretical and experimental investigation has been conducted to evaluate the fundamental supersonic aerodynamic characteristics of a generic twin-body wind-tunnel model. The experimental testing was performed in the Langley Unitary Plan Wind Tunnel at a Mach number of 2. 70. Experimental data were obtained on a simple rectangular-wing twin-body wind-tunnel model; these data were used to evaluate prediction methods and to investigate interference effects.

Original languageEnglish (US)
JournalNASA Technical Paper
Publication statusPublished - Jan 1 1983

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All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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