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GROUND AND FLIGHT TEST METHODS FOR DETERMINING LIMIT CYCLE AND STRUCTURAL RESONANCE CHARACTERISTICS OF AIRCRAFT STABILITY AUGMENTATION SYSTEMS

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BookPublisher: Nasa, Washington, D.C. 1972Description: 20.DDC classification: NASA | TN D-6867 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-6867 - (Browse shelf)	Not for loan		TR8454

Total holds: 0

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Previous	NASA TN D-6863 - APOLLO 9 THERMAL-CONTROL-COATING DEGRADATION	NASA TN D-6864 - VIBRATION AND AERODYNAMIC BUCKLING EXPERIMENTS FOR BLUNT TRUNCATED CONICAL SHELLS WITH RING SUPPORTED EDGES	NASA TN D-6865 - ANALYSIS OF THE FLOW IN A 1-MJ ELECTRIC-ARC SHOCK TUNNEL	NASA TN D-6867 - GROUND AND FLIGHT TEST METHODS FOR DETERMINING LIMIT CYCLE AND STRUCTURAL RESONANCE CHARACTERISTICS OF AIRCRAFT STABILITY AUGMENTATION SYSTEMS	NASA TN D-6868 - MASS INFLUX OBTAINED FROM LLLTV OBSERVATIONS OF FAINT METEORS	NASA TN D-6869 - ANALYTICAL STUDY OF AIRPLANE-AUTOPILOT RESPONSE TO ATMOSPHERIC TURBULENCE	NASA TN D-6870 - RING-BAFFLE PRESSURE DISTRIBUTION AND SLOSH DAMPING IN LARGE CYLINDRICAL TANKS	Next

Bound With Nasa Tn D-6860-79

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