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SUBSONIC AERODYNAMIC HEAT TRASFER TO A SURFACE RECESSED WITHIN A FORWARD STAGNATION REGION SLIT.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 9.DDC classification: NASA | TN D-2034

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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-2034 (Browse shelf)	Not for loan		TR15010

Total holds: 0

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Previous	NASA TN D-203 EXPERIMENTAL STUDY OF ZERO-FLOW ENJECTORS USING GASEOUS NITROGEN	NASA TN D-2032 MAGNETICALLY ROTATED ELECTRIC ARC AIR HEATER EMPLOYING A STRONG MAGNETIC FIELD AND COPPER ELECTRODES.	NASA TN D-2033 TRANSONIC INVESTIGATION OF DYRAMIDAL REENTRY CONFIGURATION WITH CAMBERED VARIABLE-SWEEP WINGS AND VARIOUS LONGITUDINAL CONTROLS.	NASA TN D-2034 SUBSONIC AERODYNAMIC HEAT TRASFER TO A SURFACE RECESSED WITHIN A FORWARD STAGNATION REGION SLIT.	NASA TN D-2038 EXPERMENTAL AND CALCULATED RESULTS OF A FLUTTER INVESTIGATION OF SOME VERY LOW ASPECT-RATIO FLAT-PLATE SURFACE AT MACH NUMBERS FROM 0.62 TO 3.00	NASA TN D-2039 DIFUSSION STUDIES OF SEVERAL OXIDATION RESISTANT COATINGS ON M0-05TI MOLYBDENUM ALLOY AT 2.5000 DEGREE F.	NASA TN D-204 EXPERIMENTAL DETERMINATION OF THE TEMPERATURE AND DYNAMIC-STRAIN ENVIRONMENT OF A TUBULAR COMBUSTOR LINEAR IN A TURBOJET ENGINE	Next

Bound With Nasa Tn D-2031-2036.2038-2040.

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