| 1. | Deflection angles of 50 degrees are reportedly possible without measurable deflection aberration.
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| 2. | Where \ hat { \ alpha } is the Einstein deflection angle.
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| 3. | This reduces the needed deflection angle of the aileron.
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| 4. | The reason is that deflection aberrations become large as the deflection angle increases.
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| 5. | Note that the deflection angle is proportional to 1 / v ^ 2.
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| 6. | These waves are studied to obtain a relation between deflection angle and Mach number.
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| 7. | Both France and UK introduced tachymetric devices to track targets and produce vertical and horizontal deflection angles.
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| 8. | What again causes a change in the deflection angle and has to be considered when designing the experiment.
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| 9. | An alternative way would be to calculate the deflection angle at which the boundary layer subjected to the inviscid pressure field separates.
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| 10. | If the deflection angle, e, between the guide vanes is small, the magnitude of the secondary vorticity is represented as
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