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FLOW EVALUATION IN AN ARC-HEATED HYPERSONIC WIND TUNNEL.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 30.DDC classification: NASA | TN D-2344

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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-2344 (Browse shelf)	Not for loan		TR13039

Total holds: 0

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Previous	NASA TN D-2340 HEAT-TRANSFER MEASUREMENTS ON A FLAT PLATE AND ATTACHED FINS AT MACH NUMBERS OF 3.51 AND 4.44	NASA TN D-2342 A PRARMETRIC STUDY OF HYPERSONIC FLOW FIELDS ABOUT BLUNT-NOSED CYLINDERS AT ZERO ANGLE OF ATTACK.	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.	Next

Bound With Nasa Tn D-2341-43,2345-50.

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