Demonstration of Frequency-Sweep Testing Technique Using a Bell 214-ST Helicopter

A demonstration of frequency-sweep testing using a Bell-214ST single- rotor helicopter was completed in support of the Army's development of an updated MIL-H-8501A, and an LHX (ADS-33) handling-qualities specification. Hover and level-flight condition (Va = 0 knots and Va = 90 knots) tests were...

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Bibliographische Detailangaben
Hauptverfasser:	Tischler, Mark B, Fletcher, Jay W, Diekmann, Vernon L, Williams, Robert A, Cason, Randall W
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMIC STABILITY Aerodynamics ARMY AIRCRAFT ARMY PERSONNEL AUGMENTATION CLOSED LOOP SYSTEMS DATA PROCESSING DYNAMIC RESPONSE DYNAMICS FLIGHT FLIGHT TESTING FREQUENCY FREQUENCY RESPONSE FREQUENCY SWEEP TESTING HANDLING HANDLING QUALITIES Helicopters HOVERING LEVEL FLIGHT PILOTS SINGLE MOTOR HELICOPTERS SPECIFICATIONS TEST METHODS
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