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APPLICATION OF APPROACH SPEED CRITERIA DERIVED FROM CLOSED-LOOP PILOT-VEHICLE SYSTEMS ANALYSES TO AN OGEE WING AIRCRAFT

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BookPublisher: Nasa, Washington, D.C. Description: 45.DDC classification: NASA | CR-579

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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 CR-579 (Browse shelf)	Not for loan		TR12783

Total holds: 0

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Previous	NASA CR-575 EVALUATION OF HIGH-TEMPERATURE GAS TRANSPORT PROPERTIES.	NASA CR-577 BIOLOGICAL CONTROL SYSTEMS-A CRITICAL REVIEW AND EVALUATION	NASA CR-578 PREDICTED AND MEASURED PERFORMANCE OF TWO FULL-SCALE DUCTED PROPELLERS	NASA CR-579 APPLICATION OF APPROACH SPEED CRITERIA DERIVED FROM CLOSED-LOOP PILOT-VEHICLE SYSTEMS ANALYSES TO AN OGEE WING AIRCRAFT	NASA CR-580 ISOLATION OF COMPONENTS ON A SILICON WAFER USING SIO 2	NASA CR-582 A CONTRIBUTION TO THE MICROMECHANICS OF COMPOSITE MATERIALS STRESSES AND FAILURE MECHANICSMS INDUCED BY INCLUSIONS	NASA CR-583 STUDY OF PERTURBED PERIODIC SYSTEMS OF DIFFERENTIAL QUATIONS-THE STROBOSCOPIC METHOD	Next

Bound With Nasa Cr-576-580

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