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SLR TEMPERATURE MEASUREMENTS IN THE SUPERSONIC EXPANSION OF NITROGEN IN SHOCKTUNNEL

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Material type: Text

TextSeries: Aeronautical Research Council Current Papers ; Cp No.1294Publication details: DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	CP-1294 (Browse shelf(Opens below))	Not for loan		TR3321

Total holds: 0

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Previous	CMERI A9 DESIGN OF HIGH ALTITUDE CHAMBER FOR TESTING ENGINES	CP 1283 Results of a series of wind tunnel tests on the victor B.MK.2.aircraft and a comparison with drag estimates and full scale flight data	CP-1292 SOME RESULTS OF WIND-TUNNEL TESTS ON AN AEROFOIL SECTION (NPL 9510) COMBINING A'PEAKY' UPPER SURFACE-PRESSURE DISTRIBUTION WITH REAR LOADING	CP-1294 SLR TEMPERATURE MEASUREMENTS IN THE SUPERSONIC EXPANSION OF NITROGEN IN SHOCKTUNNEL	CP-1295 PREDICTION METHOS FOR PRESSURE DISTRIBUTIONS ON COMPRESSION SURFACES OF COMICAL BODIES AT SUPERSONIC SPEEDS	CP-1296 NON-LINEAR STABILITY THEORY OF THE FLAT PLATE BOUNDARY LAYER	CP1311 THRUST/ DRAG ANALYSIS FOR A FRONT FAN NACELLE HAVING TWO SEPARATE COAXIAL EXHAUST STREAMS	Next

Bound With: Arc Cp No.-1291-1300

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