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

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
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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
Language: en
Pages: 15

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

Authors: Harold S. Johnson
Categories:
Type: BOOK - Published: 1953 - Publisher:

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WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6
Language: en
Pages: 30

WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6

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Type: BOOK - Published: 1953 - Publisher:

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Wind-tunnel Investigation at High Subsonic Speeds of Spoilers of Large Projection on an NACA 65A006 Wing with Quarter-chord Line Swept Back 32.6 Degrees
Language: en
Pages: 31

Wind-tunnel Investigation at High Subsonic Speeds of Spoilers of Large Projection on an NACA 65A006 Wing with Quarter-chord Line Swept Back 32.6 Degrees

Authors: Raymond D. Vogler
Categories:
Type: BOOK - Published: 1952 - Publisher:

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Wind-tunnel Investigation at High Subsonic Speeds of a Spoiler-slot-deflector Combination on an NACA 65A006 Wing with Quarter-chord Line Swept Back 32.6 Degrees
Language: en
Pages: 24

Wind-tunnel Investigation at High Subsonic Speeds of a Spoiler-slot-deflector Combination on an NACA 65A006 Wing with Quarter-chord Line Swept Back 32.6 Degrees

Authors: Raymond D. Vogler
Categories:
Type: BOOK - Published: 1953 - Publisher:

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Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Language: en
Pages: 692

Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds

Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1956 - Publisher:

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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