A discussion of recent wind-tunnel studies relating to the problems of estimating vertical- and horizontal-tail loads
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Kuhn, Richard E↗
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Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Complete Model with an Unswept Wing and a Sweptback Horizontal Tail at Two Vertical Locations
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Hieser, Gerald↗
Longitudinal Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Model Having a 60 Degree Delta Wing and Low Swept Horizontal Tail
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Peck, Robert F↗
Lateral-control Investigation at Transonic Speeds of Differentially Deflected Horizontal-tail Surfaces for a Configuration Having a 6-percent-thick 45 Degree Sweptback Wing
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Critzos, Chris C↗
Effect of Large Negative Dihedral of the Horizontal Tail on Longitudinal and Lateral Stability Characteristics of a Swept-wing Configuration at Transonic Speeds
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Arabian, Donald D↗
Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet
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Salmi, Reino J↗
Experimental Investigation at High Subsonic Speed of the Rolling Stability Derivatives of a Complete Model Having a Clipped-delta Wing and a High Horizontal Tail
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Sleeman, William C , Jr↗
The use of the horizontal rail for roll control
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Campbell, John P↗
Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights
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Fournier, Paul G↗
Longitudinal Stability Investigation for a Mach Number Range of 0.8 to 1.7 of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail
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Mcfall, John C , Jr↗
Investigation at high subsonic speeds of the effect of horizontal-tail location on longitudinal and lateral stability characteristics of a complete model having a sweptback wing in a high location
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Silvers, H Norman↗
Longitudinal Characteristics of an Unswept-wing Fighter-type Model with External Stores at a Mach Number of 1.82 and Some Effects of Horizontal-tail and Yaw-damper-vane Deflection on the Sideslip Derivatives
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Robinson, Ross B↗
A Transonic Wind-tunnel Investigation of Store and Horizontal-tail Loads and Some Effects of Fuselage-afterbody Modifications on a Swept-wing Fighter Airplane
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Hallissy, Joseph M , Jr↗
A transonic investigation of the static longitudinal-stability characteristics of a 45 degree sweptback wing-fuselage combination with and without horizontal tail
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Critzos, Chris C↗
Free-flight Investigation of the Control Effectiveness of a Differentially Deflected Horizontal Tail at Mach Numbers from 0.8 to 1.6
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Mitchell, Jesse L↗
Free-flight Investigation over a Mach Number Range from 0.74 to 1.43 at Lift Coefficients from Minus 0.15 to 0.75 of an Airplane-configuration Model Having a 52.5 Degree Delta Wing and a Low Swept Horizontal Tail
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Kehlet, Alan B↗
Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
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Burrows, Dale L↗
Investigation at High Subsonic Speeds of the Static Lateral and Directional Stability and Tail-loads Characteristics of a Model Having a Highly Tapered Swept Wing of Aspect Ratio 3 and Two Horizontal-tail Positions
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Few, Albert G , Jr↗