Time histories of the loads and deformations on the horizontal tail of a jet-powered bomber airplane in accelerated maneuvers at 30,000 feet
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COONEY T V↗
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Spin and recovery characteristics of a model of a fighter type of airplane without a horizontal tail having either a single vertical tail or twin vertical tails
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Gale, Lawrence J↗
Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2
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Luoma, Arvo A↗
Time Histories of Horizontal-tail Loads, Elevator Loads, and Deformations on a Jet-powered Bomber Airplane During Wind-up Turns at Approximately 15,000 Feet and 22,500 Feet
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Mcgowan, William A↗
Time histories of horizontal-tail loads and deformations on a jet-powered bomber airplane during wind-up turns at 15,000 feet and 22,500 feet
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Mcgowan, William A↗
Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface
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Draper, John W↗
Investigation of annular liquid flow with concurrent air flow in horizontal tubes
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Kinney, Goerge R↗
Tests in the Ames 40- by 80-foot Wind Tunnel of an Airplane Configuration with an Aspect Ratio 2 Triangular Wing and an All-movable Horizontal Tail : Longitudinal Characteristics
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Graham, David↗
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↗
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↗