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WIND-TUNNEL CALIBRATION AND REQUIREMENTS FOR IN-FLIGHT USE OF FIXED HEMISPHERICAL HEAD ANGLE-SIDESLIP SENSORS.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 45.DDC classification: NASA | TN D-6986

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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-6986 (Browse shelf)	Not for loan		TR11345

Total holds: 0

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Previous	NASA TN D-6983 ADHERSION AND TRANSFER OF POLYTERAFLUORETHYLENE TO METALS STUDIED BY AUGER EMISSION SPECTROSCOPY.	NASA TN D-6984 EFFECTIVE SPECIFIEC IMPULSE OF EXTERNAL NUCLEAR PULSE PROPULSION SYSTEMS.	NASA TN D-6985 ION HEATING MECHANISM IN A MODIFIED PENNING DISCHARGE.	NASA TN D-6986 WIND-TUNNEL CALIBRATION AND REQUIREMENTS FOR IN-FLIGHT USE OF FIXED HEMISPHERICAL HEAD ANGLE-SIDESLIP SENSORS.	NASA TN D-6987 LOCAL FLOW MEASUREMENTS AT THE INLET SPIKE TIP OF A MACH 3 SUPERSONIC CRUISE AIRPLANE.	NASA TN D-6988 EFFECT OF AGING AT 1040DEGREE C (1900DEGREE F) ON THE DUCTILITY AND STRUCTURE OF A TANTALUM ALLOY, T-111.	NASA TN D-6989 MULTIMATERIAL LAMINATION AS A MEANS OF RETARDING PENETRATION AND SPLLATION FAILURES IN PLATES.	Next

Bound With Nasa Tn D-6980-6985,6987-89.

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