Time histories of the aerodynamic loads on the vertical and horizontal tail surfaces of a jet-powered bomber airplane during sideslip maneuvers at approximately 20,000 feet
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Cooney, T V↗
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Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87
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Mayer, John P↗
Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 5.5 x 10(exp 6) of a circular-arc 52 degrees sweptback wing with a fuselage and a horizontal tail at various vertical positions
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Foster, Gerald V↗
Investigation in the Ames 12-foot Pressure Wind Tunnel of a Model Horizontal Tail of Aspect Ratio 3 and Taper Ratio 0.5 Having the Quarter-chord Line Swept Back 45 Degrees
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Kolbe, Carl D↗
Summary of results of a wind-tunnel investigation of nine related horizontal tails
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Dods, Jules B , Jr↗
The unsymmetrical load and bending moment on the horizontal tail of a jet-powered bomber measured in sideslipping flight
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Cooney, T V↗
An Investigation of the Longitudinal Characteristics of the X-3 Configuration with Wing and Horizontal Tail Surfaces of Aspect Ratio 3.0 by Means of Rocket-propelled Models : Results at High Lift Coefficients
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Peck, Robert F↗
Tests in the Ames 40- by 80-foot Wind Tunnel of an Airplane Configuration with an Aspect Ratio 4 Triangular Wing and an All-movable Horizontal Tail - Longitudinal Characteristics
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Graham, David↗
Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 6.0 x 10(exp 6) of a 52 degree sweptback wing equipped with various spans of leading-edge flaps, a fuselage, and a horizontal tail at various vertical positions
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Griner, Roland F↗
Investigation of a Triangular Wing in Conjunction with a Fuselage and Horizontal Tail to Determine Downwash and Longitudinal-stability Characteristics : Transonic Bump Method
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Allen, Edwin C↗
Full-scale Wind-tunnel Investigation of the Effects of Wing Modifications and Horizontal-tail Location on the Low-speed Static Longitudinal Characteristics of a 35 Degree Swept-wing Airplane
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Maki, Ralph L↗
Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback-wing-fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Salmi, Reino J↗
Use of an Aerodynamically Pulsed All-movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-powered Models in Free Flight and Some Initial Results from an Arrow-wing-body-tail Configuration
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Gillespie, Warren, Jr↗
Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails
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Jaquet, Byron M↗
Longitudinal Stability, Trim, and Drag Characteristics of a Rocket-propelled Model of an Airplane Configuration Having a 45 Degree Sweptback Wing and an Unswept Horizontal Tail
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Parks, James H↗
Preliminary Results of Horizontal-tail Load Measurements of the Bell X-5 Research Airplane
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Rogers, John T↗
A study of the flow field behind the triangular horizontal tail of a canard airplane at approximately the vertical-tail location by means of a tuft grid
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Johnson, Joseph L , Jr↗
Effects of Twist and Camber, Fences, and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristics of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Foster, Gerald V↗