Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. : Taper-ratio series /
An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of variations in taper ratio within the range of 0.3 to 1.0 on the static lateral stability characteristics at high subsonic speeds of wing-fuselage combinations having wings of 45 degrees sweepbac...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4174 |
| Subjects: | |
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| Summary: | An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of variations in taper ratio within the range of 0.3 to 1.0 on the static lateral stability characteristics at high subsonic speeds of wing-fuselage combinations having wings of 45 degrees sweepback at the quarter-chord line and an aspect ratio of 4 |
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| Item Description: | NACA TN No. 4174 |
| Physical Description: | 25 p. : ill ; 27 cm |
| Bibliography: | Includes bibliographical references |