Publication Date:
2019-07-11
Description:
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a booster incorporated in the elevator control system. Tests were made to determine the effects on the handling qualities of the test airplane of variations in pilots control-force gradients as well as the effects of variations in the maximum rate of control motion supplied by the booster system.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-L50D11
,
Rept-3130
Format:
application/pdf
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