A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslip
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Letko, William↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Low-speed investigation of the aerodynamic, control and hinge-moment characteristics in sideslip of a delta-wing-fuselage model with horn-balance-type ailerons and with and without nacelles
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Scallion, William I↗
Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing fuselage combination having a triangular wing of aspect ratio 4
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Fournier, Paul G↗
An analytical study of sideslip angles and vertical-tail loads in rolling pullouts as affected by some characteristics of modern high-speed airplane configurations
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Stone, Ralph W , Jr↗
Wind-tunnel Investigation of the Effects of Geometric Dihedral on the Aerodynamic Characteristics in Pitch and Sideslip of an Unswept- and a 45 Degree Sweptback-wing-fuselage Combination at High Subsonic Speeds
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Kuhn, Richard E↗
An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7
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Christensen, Frederik B↗
Wind-tunnel investigation at a Mach number of 2.01 of the aerodynamic characteristics in combined pitch and sideslip of some canard-type missiles having cruciform wings and canard surfaces with 70 degree delta plan forms
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Spearman, M Leroy↗
An Investigation at High Subsonic Speeds of the Pressure Distributions on a 45 Degree Sweptback Vertical Tail in Sideslip with and Without a 45 Degree Sweptback Horizontal Tail Located on the Fuselage Center Line
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Wiley, Harleth G↗
Aerodynamic loading characteristics in sideslip of a 45 degree sweptback wing with and without a fence at high subsonic speeds
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Kuhn, Richard E↗
Effects of Free-flight Rocket-model Booster-adapter Configurations on the Aerodynamic Characteristics in Pitch and Sideslip of a Swept-wing Fighter Airplane Model at a Mach Number of 2.01
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Robinson, Ross B↗
Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail : Basic-data Presentation, M = 2.01
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Spearman, M Leroy↗
The rolling moment due to sideslip of swept wings at subsonic and transonic speeds
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Polhamus, Edward C↗
Experimental Determination of the Aerodynamic Derivatives Arising from Acceleration in Sideslip for a Triangular, a Swept, and an Unswept Wing
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Riley, Donald R↗
Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of the Wing and Horizontal Tail : Effect of Wing Location and Geometric Dihedral for the Wing-body Com
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Spearman, M Leroy↗
An Investigation at High Subsonic Speeds of the Effects of Horizontal-tail Height on the Aerodynamic and Loading Characteristics in Sideslip on a 45 Degree Sweptback, Untapered Tail Assembly as Determined from Force Tests and Integrated Vertical-tail Span Loadings
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Wiley, Harleth G↗
Effect of automatic stabilization on the sideslip and angle-of-attack disturbances in rolling maneuvers
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Gates, Ordway B , Jr↗
Some factors affecting the variation of pitching moment with sideslip of aircraft configurations
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Polhamus, Edward C↗
Wind-tunnel Investigation at Low Speed of Sideslipping, Rolling, Yawing, and Pitching Characteristics for a Model of a 45 Degree Swept-wing Fighter-type Airplane
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Jaquet, Byron M↗