Acceleration restrictor which limits elevator motion of aircraft is analyzed by means of electronic analog computer.
Theoretical analysis of airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity
NACA -- Tech Note
1954
42 pages
Report
Englisch
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Numerical Representation of Pitching and Non-Pitching Airfoils Undergoing Linear Acceleration
British Library Conference Proceedings | 1997
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