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

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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Total Pages: 30
Release: 1953
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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

Authors:
Categories:
Type: BOOK - Published: 1953 - 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 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 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 to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Language: en
Pages: 36

Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives

Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

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