Wind Tunnel Investigation At High Subsonic Speeds Of The Effect Of Spoiler Profile On The Lateral Control Characteristics Of A Wing Fuselage Combination Winter Quarter Chord Line Swept Back 326c And Naca 65a006 Airfoil Section
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Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section
Author | : Harold S. Johnson |
Publisher | : |
Total Pages | : 15 |
Release | : 1953 |
Genre | : |
ISBN | : |
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Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section Related Books
Language: en
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An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral