Experimental And Predicted Longitudinal Response Characteristics Of A Large Flexible 35 Degree Swept Wing Airplane At An Altitude Of 35000 Feet

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Experimental and Predicted Longitudinal Response Characteristics of a Large Flexible 35 Degree Swept-wing Airplane at an Altitude of 35,000 Feet
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Experimental and Predicted Longitudinal and Lateral-directional Response Characteristics of a Large Flexible 35̊ Swept-wing Airplane at an Altitude of 35,000 Feet
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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
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Calculated simplified transfer function coefficients based on the lateral-directional equations of motion are compared with coefficients obtained by matching tr
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Comparison of Several Methods for Estimating Low-speed Stability Derivatives for Two Airplane Configurations
Language: en
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Methods presented in five different publications have been used to estimate the low-speed stability derivatives of two unpowered airplane configurations. One co