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EXPERIMENTAL AND THEORETICAL TURBULENT BOUNDARY LAYER DEVELOPMENTIN A MACH 4.4 WATER-COOLED CONICAL NOZZLE

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BookPublisher: Nasa, Washington, D.C. 1969Description: 41.DDC classification: NASA | TN D-5377 -

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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-5377 - (Browse shelf)	Not for loan		TR9341

Total holds: 0

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Previous	NASA TN D-5374 - CAUSES, MEASUREMENT, AND ELIMINATION OF FUEL-ELEMENT FISSION PRODUCT LEAKAGE AT THE NASA PLUM BROOK REACTOR	NASA TN D-5375 - EFFECT OF INJECTION ELEMENT RADIAL DISTRIBUTION AND CHAMBER GEOMETRY ON ACOUSTIC-MODE INSTABILITY IN A HYDROGEN OXYGEN ROCKET	NASA TN D-5376 - OXIDATION AND THERMAL FATIGUE CRACKING OF NICKEL-AND COBALT-BASE ALLOYS IN A HIGH VELOCITY GAS STREAM	NASA TN D-5377 - EXPERIMENTAL AND THEORETICAL TURBULENT BOUNDARY LAYER DEVELOPMENTIN A MACH 4.4 WATER-COOLED CONICAL NOZZLE	NASA TN D-5378 - AERODYNAMIC CHARACTERISTICS IN PITCH OF A 1/7-SCALE MODEL OF A TWO- AND THREE-STAGE ROCKET CONFIGURATION AT MACH NUMBERS OF 0.4 TO 4.63	NASA TN D-5379 - AERODYNAMIC INTERFERENCE EFFECTS CAUSED BY PARALLEL-STAGED SIMPLE AERODYNAMIC CONFIGURATIONS AT MACH NUMBERS OF 3 AND 6	NASA TN D-538 A STUDY OF THE FEASIBILITY OF INFLATABLE REENTRY GLIDERS	Next

Bound With Nasa Tn D-5371-80

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