Restrictor is intended to be applicable to airplanes having stable and reasonably linear pitching-moment characteristics; adjusted results of tests made indicated that acceleration restrictor of type described could limit peak acceleration to about 1.15 times present value by use of proper signal gains and for conditions tested.
Flight investigation of acceleration restrictor
NASA -- Tech Note
1960
29 pages
Report
English
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A flight investigation of an acceleration restrictor
TIBKAT | 1960
|Engineering Index Backfile | 1954
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