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LOW-SPEED LONGITUDINAL AERODYNAMIC INVESTIGATION OF PARAWINGS AS AUXILILIARY LIFTING DEVICES FOR A SUPERSONIC AIRPLANE CONFIGURATION.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 53.DDC classification: NASA | TN D-2346

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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-2346 (Browse shelf)	Not for loan		TR13041

Total holds: 0

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Previous	NASA TN D-2343 THE CAPABILITY OF A PROPORATIONAL-TYPE LATERAL CONTROL SYSTEM IN PROVIDING AERDYNAMIC HEADING-ANGLE TRAJECTORY CONTROL DURING REENTRY.	NASA TN D-2344 FLOW EVALUATION IN AN ARC-HEATED HYPERSONIC WIND TUNNEL.	NASA TN D-2345 EXPERIMENTAL EVIDENCE OF DEGRADATION EFFECTS IN SHORT SAMPLES OF HARD SUPERCONDUCTORS.	NASA TN D-2346 LOW-SPEED LONGITUDINAL AERODYNAMIC INVESTIGATION OF PARAWINGS AS AUXILILIARY LIFTING DEVICES FOR A SUPERSONIC AIRPLANE CONFIGURATION.	NASA TN D-2347 SPECTROGRAPHIC DATA OBTAINED FROM REENTRES AT 10.9 AND 8.1 KILLOMETERS PER SECOND OF TWO STAGES OF TAILBLAZER IIB.	NASA TN D-2348 FUSED FLUORIDE COATINGA AS SOLID LUBRICANTS IN LIQUID SODIUM, HYDROGEN.VACUUM,AND AIR.	NASA TN D-2349 LOW-SUBSONIC AERDYNAMIC AHARACTERISTICS OF A DELTA-WING RECOVERY DEVICE.	Next

Bound With Nasa Tn D-2341-45,2347-50.

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