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Experimental and Predicted Lateral-directional Dynamic-response Characteristics of a Large Flexible 35 Degree Swept-wing Airplane at an Altitude of 35,000 Feet
Calculated simplified transfer function coefficients based on the lateral-directional equations of motion are compared with coefficients obtained by matching transient time histories with an analog computer. Aerodynamic derivatives extracted from measured transfer function coefficients are also compared with estimated derivatives. In general, good agreement between measured and estimated values was obtained.
NASA Technical Note
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