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

Richard M. Wood; David S. Miller; Kenneth S. Brentner

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

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

Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

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 language	English (US)
Journal	NASA Technical Paper
State	Published - 1983

All Science Journal Classification (ASJC) codes

Aerospace Engineering

Cite this

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title = "THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWIN-FUSELAGE CONCEPT.",

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.",

author = "Wood, \{Richard M.\} and Miller, \{David S.\} and Brentner, \{Kenneth S.\}",

year = "1983",

language = "English (US)",

journal = "NASA Technical Paper",

issn = "0148-8341",

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TY - JOUR

T1 - THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWIN-FUSELAGE CONCEPT.

AU - Wood, Richard M.

AU - Miller, David S.

AU - Brentner, Kenneth S.

PY - 1983

Y1 - 1983

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/85040305430

UR - https://www.scopus.com/pages/publications/85040305430#tab=citedBy

M3 - Article

AN - SCOPUS:85040305430

SN - 0148-8341

JO - NASA Technical Paper

JF - NASA Technical Paper

ER -

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

Abstract

All Science Journal Classification (ASJC) codes

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