Investigation at transonic speeds of deflectors and spoilers as gust alleviators on a 35 degree swept wing. : Transonic bump method /
An investigation was made in the Langley high-speed 7- by 10-foot tunnel by means of the transonic-bump method to determine the gust-alleviation capabilities of spoilers and deflectors when mounted on a 35 degree swept semispan wing having NACA 65A006 airfoil sections. The Mach number range was frcm...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4006 |
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| Call Number: |
NACA TN 4006 |
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