Effects of Propeller Operation and Angle of Yaw on the Distribution of the Load on the Horizontal Tail Surface of a Typical Pursuit Airplane
No abstract available
TAIL SURFACES-CURTISS P-40K-WIND TUNNEL TESTS(NACA↗
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An Investigation of the Mutual Interference Effects of a Tail-surface : Stern Propeller Installation on a Model Simulating the Douglas XB-42 Empennage
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TAIL SURFACES - DOUGLAS B-42 - WIND TUNNEL TESTS (↗
Wind-tunnel tests of spoilers on tail surfaces
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AIRPLANES, TORPEDO↗
Wind-Tunnel Investigation of a Section of the Horizontal Tail Surface for the Bell XP-63 Airplane
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AIRFOILS - NACA 66,2X-009 (MODIFIED) - CHAR , MOME↗
Theoretical method for solution of aerodynamic forces on thin wings in nonuniform supersonic stream with an application to tail surfaces
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THEORIES - WINGS↗
Flight Tests of Various Tail Modifications on the Brewster XSBA-1 Airplane I : Measurements of Flying Qualities with Original Tail Surfaces
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AIRPLANES - BREWSTER SBA-1 FLIGHT TESTS (EXPERIMEN↗
Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface
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WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')↗
Investigation at High Subsonic Speeds of the Use of Low Auxiliary Tail Surfaces Having Dihedral to Improve the Longitudinal and Directional Stability of a T-tail Model at High Lift
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Sleeman, William C , Jr↗
Aerodynamic characteristics of thin empirical profiles and their application to the tail surfaces and ailerons of airplanes
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AIRFOILS, THIN - CHARACTERISTICS↗
Stability and Control Characteristics at Low Speed of an Airplane Model Having a 38.7 Degree Sweptback Wing with Aspect Ratio 4.51, Taper Ratio 0.54, and Conventional Tail Surfaces
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FINS, VENTRAL↗
Wind-Tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane
No abstract available
TABS, ELEVATOR - GRUMMAN TBF-1↗
Effect of Fabric Deflection at High Speeds on the Aerodynamic Characteristics of the Horizontal Tail Surface of an SB2D-1 Airplane
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ELEVATORS-HINGE MOMENTS↗
Air-Flow Surveys in the Region of the Tail Surfaces of a Single-Engine Airplane Equipped with Dual-Rotating Propellers
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PROPELLERS - WIND TUNNEL TESTS↗
The Effect on Stability and Control of a Pusher Propeller Behind Conventional Tail Surfaces as Determined by Tests of a Powered Model in the Free-flight Tunnel
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PROPELLERS, PUSHER VS TRACTOR↗
Lifting-surface-theory aspect-ratio corrections to the lift and hinge-moment parameters for full-span elevators on horizontal tail surfaces
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Swanson, Robert S↗
Experimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degree Sweptback Wing and Tail Surfaces
An investigation was made to determine the effects of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with wing and vertical tails having the quarter-chord lines swept back 45 degrees. The results indicate that the directional instability of the various isolated fuselages was about two-thirds as large as that predicted by classical theory.
Queijo, M J↗
Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps
A method of calculating the horizontal tail area for an airplane equipped with flaps is presented.. The general problem of tail design, the effects of flaps on the factors involved, and the manner in which the flaps change the requirements upon which the minimum horizontal tail area is based are discussed.
Soule, Hartley A↗
Investigation of aerodynamic characteristics at high subsonic speeds of two supersonic- cruise airplane configurations having tail surfaces outboard of the wing tips
Subsonic stability and control characteristics of two outboard-tail supersonic-cruise airplane configurations
STABILITY AND CONTROL↗