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24-ft tunnel tests on a high-lift model: Downwash and velocity measurements at the tailplane

24-ft tunnel tests on a high-lift model: Downwash and velocity measurements at the tailplane

by AERONAUTICAL RESEARCH COUNCIL

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Wing flow measurements of the damping in pitch derivative of a 45degree delta wing-body combination and with a tailplane in two positions

Wing flow measurements of the damping in pitch derivative of a 45degree delta wing-body combination and with a tailplane in two positions

by AERONAUTICAL RESEARCH COUNCIL

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Effect of Twin Fins on Isolated Tailplane Lift-curve Slope. 91009

Effect of Twin Fins on Isolated Tailplane Lift-curve Slope. 91009

by Unknown Author

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Fixture Designing For Aircraft Tailplane Eyebolt: Development of Shop made Boring Fixture for Machining of Tailplane Eyebolt

Fixture Designing For Aircraft Tailplane Eyebolt: Development of Shop made Boring Fixture for Machining of Tailplane Eyebolt

by Prabhu Rao

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An aerodynamic study of sailplane horizontal tailplane configurations and sizing (Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1976. M.S)

An aerodynamic study of sailplane horizontal tailplane configurations and sizing (Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1976. M.S)

by Vlado Lenoch

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Fatigue loadings in flight: Loads in the tailplane and fin of a Varsity

Fatigue loadings in flight: Loads in the tailplane and fin of a Varsity

by AERONAUTICAL RESEARCH COUNCIL

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Fatigue loadings in flight-loads in the tailplane of a Devon

Fatigue loadings in flight-loads in the tailplane of a Devon

by AERONAUTICAL RESEARCH COUNCIL

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Contribution of Fin to Sideforce,Yawing Moment and Rolling Moment Derivatives Due to Sideslip,(Y Sub V) Sub F,(N Sub V) Sub F,(L Sub V) Sub F,in the Presence of Body,Wing and Tailplane. 82010

Contribution of Fin to Sideforce,Yawing Moment and Rolling Moment Derivatives Due to Sideslip,(Y Sub V) Sub F,(N Sub V) Sub F,(L Sub V) Sub F,in the Presence of Body,Wing and Tailplane. 82010

by Unknown Author

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Tests on a Hunter F.2 of two strain gauge methods for measuring tailplane loads in flight, with some loads measured in level flightpitch-ups and transonic dives

Tests on a Hunter F.2 of two strain gauge methods for measuring tailplane loads in flight, with some loads measured in level flightpitch-ups and transonic dives

by Aeronautical Research Council (Great Britain)

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Dhc-6 Twin Otter Tailplane Airfoil Section Testing in the Ohio State University 7x10 Wind Tunnel. Volume 1

Dhc-6 Twin Otter Tailplane Airfoil Section Testing in the Ohio State University 7x10 Wind Tunnel. Volume 1

by National Aeronautics and Space Administration

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Low-speed tunnel model tests on tailplane rolling monments in sideslip

Low-speed tunnel model tests on tailplane rolling monments in sideslip

by AERONAUTICAL RESEARCH COUNCIL

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Contribution of Fin and Tailplane to Sideforce and Yawing Moment Derivatives Due to Sideslip at Supersonic Speeds at Low Angle of Attack. 91031

Contribution of Fin and Tailplane to Sideforce and Yawing Moment Derivatives Due to Sideslip at Supersonic Speeds at Low Angle of Attack. 91031

by Unknown Author

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Contribution of Body-mounted Fins and Tailplanes to Lateral Derivatives Due to Sideslip at Subsonic Speeds for General Body Width to Height Ratio. 93007

Contribution of Body-mounted Fins and Tailplanes to Lateral Derivatives Due to Sideslip at Subsonic Speeds for General Body Width to Height Ratio. 93007

by Unknown Author

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Contribution of Fin to Sideforce,Yawing Moment and Rolling Moment Derivatives Due to Rate of Roll,(Y Sub P) Sub F,(N Sub P) Sub F,(L Sub P) Sub F,in the Presence of Body,Wing and Tailplane. 83006

Contribution of Fin to Sideforce,Yawing Moment and Rolling Moment Derivatives Due to Rate of Roll,(Y Sub P) Sub F,(N Sub P) Sub F,(L Sub P) Sub F,in the Presence of Body,Wing and Tailplane. 83006

by Unknown Author

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The effects of structural flexibility of tailplane, elevator, and fuselage on longitudinal control and stability, (A.R.C. technical report)

The effects of structural flexibility of tailplane, elevator, and fuselage on longitudinal control and stability, (A.R.C. technical report)

by A. R Collar

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Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights (Aeronautical Research Council. Reports and memoranda)

Subsonic wind-tunnel tests on a crescent-winged aircraft, including tests of leading-edge droop designs and several tailplane heights (Aeronautical Research Council. Reports and memoranda)

by C. N Hall

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Fatigue loadings in flight: Loads in the tailplane and fin of a Jet Provost

Fatigue loadings in flight: Loads in the tailplane and fin of a Jet Provost

by AERONAUTICAL RESEARCH COUNCIL

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