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FLIGHT EVALUATION OF ANGLE OF ATTACK AS A CONTROL PARAMETER IN GENERAL-AVIATION AIRCRAFT

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BookPublisher: Nasa, Washington, D.C. 1971Description: 22.DDC classification: NASA | TN D-6210 -

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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-6210 - (Browse shelf)	Not for loan		TR10387

Total holds: 0

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Previous	NASA TN D-6207 - ENERGY TRANSFER RATES OF AN INTEGRATED LIFE SUPPORT SYSTEM DURING MANNED AND INTERMITTENTLY MANNED TESTS	NASA TN D-6208 - EXPERIENCE WITH THE X-15 ADAPTIVE FLIGHT CONTROL SYSTEM	NASA TN D-6209 - VARIANCE REDUCTION BY IMPROTANCE SAMPLING AND THE METHOD OF SPLITING IN MONTE CARLO CALCULATIONS	NASA TN D-6210 - FLIGHT EVALUATION OF ANGLE OF ATTACK AS A CONTROL PARAMETER IN GENERAL-AVIATION AIRCRAFT	NASA TN D-6211 - EFFECT OF HYDROGEN ON TENSILE PROPERTIES OF PALLADIUM-HYDROGEN SYSTEM	NASA TN D-6212 - TWO-PHASE HYDROGEN DENSITY MEASUREMENTS USING AN OPEN-ENDED MICROWAVE CAVITY	NASA TN D-6213 - RANDOMLY FLUCTUATING FLOW IN A CHANNEL DUE TO RANDOMLY FLUCTUATING PRESSURE GRADIENTS	Next

Bound With Nasa Tn D-6200-19

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