A Simplified method for determining from flight data the rate of change of yawing-moment coefficients with sideslip /
A method is presented by which the directional stability derivated, the rate of change of yawing-moment coefficients with sidslip angle, can be evaluated for a conventional airplane from flight records of a lateral or directional oscillation. For the method shown, the calculation for a particular hi...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1946
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1076 |
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| Call Number: |
ISIL:US-CST NACA TN 1076 |
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