| 1. | Longitudinal stability could be ensured or improved by minimizing the latter effect.
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| 2. | These changes improved longitudinal stability, especially when the aircraft was fully loaded.
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| 3. | The evidence on the longitudinal stability of attachment security is therefore currently inconclusive.
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| 4. | The aerodynamic center is the conceptual starting point for longitudinal stability.
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| 5. | A wing with a conventional aerofoil profile makes a negative contribution to longitudinal stability.
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| 6. | Longitudinal stability and control may be obtained with other wing configurations, including tailless aircraft.
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| 7. | Depending on its design, a canard surface may increase or decrease longitudinal stability of the aircraft.
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| 8. | The initial flights looked at longitudinal stability and control, wing and tail loads, and pressure distribution.
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| 9. | Its purpose was to provide automatic lateral and longitudinal stability in the event of a momentary sideslip.
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| 10. | Lachmann was also concerned about longitudinal stability and included a novel moving tailplane-elevator combination for greater pitch control.
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