Analysis of flight data to determine wing fuselage aerodynamics center position, zero lift pitching moment coefficients, aircraft pitching moment of inertia, and radius of gyration; pitching moment of inertia determined from flight data for rigid wing conditions agreed with calculations based on ground tests.
Analysis of horizontal-tail loads in pitching maneuvers on flexible swept-wing jet bomber
NACA -- Tech Note
1957
58 pages
Aufsatz (Zeitschrift)
Englisch
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