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REAL-AIR DATA-REDUCTION PROCEDURES BASED ON FLOW PARAMETERS MEASURED IN THE TEST SECTION OF SUPERSONIC AND HYPERSONIC FACILITIES

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BookPublisher: Nasa, Washington, D.C. 1972Description: 90.DDC classification: NASA | TN D-6618 -

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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-6618 - (Browse shelf)	Not for loan		TR9713

Total holds: 0

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Previous	NASA TN D-6615 - EFFECTS OF REYMONDS NUMBER AND BODY CORNER RADIUS ON AERODYNAMIC CHARACTERISTICS OF A SPACE SHUTTLE-TYPE VEHICLE AT SUBSONIC MACH NUMBERS	NASA TN D-6616 - CONCEPTUAL DESIGN AND ANALYSIS OF AN INFRARED HORIZON SENSOR WITH COMPENSATION FOR ATMOSPHERIC VARIABILITY	NASA TN D-6617 - ELECTROSTATIC-PROBE MEASUREMENTS OF PLASMA PARAMETERS FOR TWO REENTRY FLIGHT EXPERIMENTS AT 25000 FEET PER SECOND	NASA TN D-6618 - REAL-AIR DATA-REDUCTION PROCEDURES BASED ON FLOW PARAMETERS MEASURED IN THE TEST SECTION OF SUPERSONIC AND HYPERSONIC FACILITIES	NASA TN D-6619 - INVESTIGATION OF SONIC BOOM GENERATED BY THIN, NONLIFTING, RECTANGULAR WINGS	NASA TN D-6621 ANALYSIS OF HEAT TRANSFER IN A POROUS COOLED WALL WITH VARIABLE PRESSURE AND TEMPERATURE ALONG THE COOLANT EXIT BOUNDARY	NASA TN D-6622 THREE-DIMENSIONAL POTENTIAL AND CURRENT DISTRIBUTIONS IN HALL GENERATOR WITH ASSUMED VELOCITY PROFILES	Next

Bound With Nasa Tn D-6610-19

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