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EVALUATION OF THE EFFECT OF A YAW-RATE DAMPER ON THE FLYING QUALITIES OF A LIGHT TWIN-ENGINE AIRPLANE

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BookPublisher: Nasa, Washington, D.C. 1970Description: 46.DDC classification: NASA | TN D-5890

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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-5890 (Browse shelf)	Not for loan		TR11768

Total holds: 0

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Previous	NASA TN D-5888 DEVELOPMENT OF A MODEL FOR DISTRIBUTED SATURATION CHARACTERISTICS IN INTEGRATED DEVICES	NASA TN D-5889 DESIGN EVALUATION OF DISTRIBUTED SATURATION CHARACTERISTICS IN INTEGRATED DEVICES	NASA TN D-589 ELECTRIC SPARK IGNITION IN CARBON-VANE FUEL PUMPS	NASA TN D-5890 EVALUATION OF THE EFFECT OF A YAW-RATE DAMPER ON THE FLYING QUALITIES OF A LIGHT TWIN-ENGINE AIRPLANE	NASA TN D-5893 - MODEL WIND-TUNNEL AND FLIGHT INVESTIGATION OF A PARAWING-LIFTING-BODY LANDING SYSTEM	NASA TN D-5894 - THE SIMULATION OF IONOSPERIC CONDITONS FOR SPACE VEHICLES	NASA TN D-5895 - EXPERIMENTAL INVESTIGATIO OF CLOSE-RANGE ROCKET-EXHAUST IMPINGEMENT ON SURAFCES IN A VACUUM	Next

Bound With Nasa Tn D-5881-5889

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