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To accommodate carrier operations, the landing gear was designed to withstand landings with a sink rate of 23 ft/s (7 m/s), while the nose strut could extend by some 20 in (50 cm) to increase angle of attack at takeoff.
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Starting at the trailing edge of the wing separation increases with increasing angle of attack.
Notice that the average emissivity gradually decreases with increasing angle away from normal incidence.
With increasing angle α, a tilting of the hysteresis loops is observed.
Conversely, discharge currents decreased with increasing angle of the needle cone.
However, the optimal angle is 0° for Scheme-II, because band gap decreases monotonically until disappears with the increasing angle.
The 'bad'-state probability increases with increasing angle between satellite azimuth and driving direction within the interval 0°…90°.
For this high lift configuration at low Mach number, the local extension grows with increasing angle of attack.
The relative deviations of emissivity from θ = 0° for increasing angle θ are listed in Table 3.
The following observations can be made in Figure13: The 'bad'-state probability increases with increasing angle between satellite azimuth and driving direction within the interval 0°…90°.
At angles equal or larger than 2° all females exhibited clear steering towards the speaker side and their steering response increased with increasing angle of incidence up to 30°, the maximum angle tested.
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