To extract stability derivative from flight test data, moments and product of inertia were measured on F-106A aircraft; spring oscillation method used gave valid results for pitching and rolling moments of inertia and for inclination of principal axes; yawing moments of inertia were not satisfactory; combination of experimental results with analytical methods used to produce final set of moments and product of inertia; new approach to experimental problem described. (Received Sept 1960)
Measurement of aircraft moments of inertia
AGARD -- Report
AGARD -- Reports ; n 248
1959
1959 pages
Report
English
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