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