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REAL-GAS INVISCID NOZZLE CONTOURS FOR NITROGEN AT MACH 15, 17, AND 19 WITH TABULATED PROPERTIES FOR THE CALCULATION OF BOUNDARY-LAYER EFFECTS

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BookPublisher: Nasa, Washington, D.C. 1964Description: 124.DDC classification: NASA | TN D-2496 -

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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-2496 - (Browse shelf)	Not for loan		TR10104

Total holds: 0

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Previous	NASA TN D-2487 A SERIES SOLUTION FOR SOME PERIODIC ORBITS IN THE RESTRICTED THREE-BODY PROBLEM ACCORDING TO THE PERTURBATION METHOD.	NASA TN D-2488 LONGITUDINAL CHRACTERISTICS OF SEVERAL CONFIGURATIONS AT HYPERSONIC MAC NUMBERS IN CONICAL AND CONTOURED NOZZELS.	NASA TN D-2493 - EVALUATION OF SELECTED ERFRACTORY OXIDE MATERIALS FOR USE IN HIGH-TEMPERATURE PEBBLE-BED WIND-TUNNEL HEAT EXCHANGERS	NASA TN D-2496 - REAL-GAS INVISCID NOZZLE CONTOURS FOR NITROGEN AT MACH 15, 17, AND 19 WITH TABULATED PROPERTIES FOR THE CALCULATION OF BOUNDARY-LAYER EFFECTS	NASA TN D-25 - Large-scale wind-tunnel tests of an airplane model with an unswept ,aspect-ratio-10 wing,four propellers ,and blowing flaps	NASA TN D-2525 NASA ENGINEERING MODELS OF THE MARS ATMOSPHERE FOR ENTRY VEHICLE DESIGN	NASA TN D-2552 LARGE-SCALE WIND-TUNNEL TESTS ON AN ASPECT RATIO 2.17 DELTA-WING MODEL EQUIPPED WITH MIDCHORD BOUNDARY-LAYER-CONTROL FLAPS.	Next

Bound With Nasa Tn D-2491-2500

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