EXPERIMENTAL DETERMINATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE LATERAL STABILITY DERIVATIVES FOR A DELTA, A SWEPT, AND AN UNSWEPT WING OSCILLATING IN YAW

Three wing models were oscillated in yaw about their vertical axes to determine the effects of systematic variations of frequency and amplitude of oscillation on the in-phase and out-of-phase combination lateral stability derivatives resulting from this motion. The tests were made at low speeds for...

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Bibliographische Detailangaben

1. Verfasser:	FISHER, LEWIS R
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft OSCILLATION ROLL WINGS YAW
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