Static Lateral Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 080 Chord Line Unswept And With Several Tail Configuration
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An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing h
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An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspectratio-3.50 wing ha
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The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the
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