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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

Raymond D. Vogler

Published: 1953

Total Pages: 24

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

Published: 1953

Total Pages: 30

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

Raymond D. Vogler

Published: 1952

Total Pages: 31

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

Harold S. Johnson

Published: 1953

Total Pages: 15

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

James W. Wiggins

Published: 1954

Total Pages: 36

Wind-tunnel Investigation at High Subsonic Speeds of the Effects of Wing-mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage

H. Norman Silvers

Published: 1954

Total Pages: 36

Wind-tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross-section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing

Thomas J. Jr King

Published: 1956

Total Pages: 61

Wind-tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 2.31 and an NACA 65A003 Airfoil

James W. Wiggins

Published: 1953

Total Pages: 28

A Transonic-wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at Mach Numbers of 1.2

Raymond B. Wood

Published: 1951

Total Pages: 43

Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences

James A. Weilberg

Published: 1952

Total Pages: 64