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PRELIMINARY EXPERIMENTAL INVESTIGATION OF LOW-SPEED TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS

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BookSeries: National Advisory Committee For Aeronautics Tn-3031. Publisher: Naca, Washington 1953Description: 37.DDC classification: TR | NACA-3031

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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	TR NACA-3031 (Browse shelf)	Not for loan		TR3533

Total holds: 0

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Previous	TR N-74 The design of a multi-cell box in pure bending for minimum weight	TR N-78 Water injection in the normally-aspirated poston engine	TR NACA-2960 DRAG OF CIRCULAR CYLINDERS FOR A WIDE RANGE OF REYNOLDS MEMBERS AND MACH NUMBERS	TR NACA-3031 PRELIMINARY EXPERIMENTAL INVESTIGATION OF LOW-SPEED TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS	TR NACA-3032 AN ANALYTICAL STUDY OF THE EFFECT OF AIRPLANE WAKE ON THE LATERAL DISPERSION OF AERIAL SPRAYS	TR NACA-3033 APPLICATION OF AN ELECTRO-OPTICAL TWO-COLOR PYROMETER TO MEASUREMENT OF FLAME TEMPERATURE FOR LIQUID OXYGEN-HYDROCARBON PROPELLANT COMBINATION	TR NACA-3034 GRAPHICAL SOLUTION OF SOME AUTOMATIC-CONTROL PROBLEMS INVOLVING SATURATION EFFECTS WITH APPLICATION TO YAW DAMPERS FOR AIRCRAFT	Next

Bound With: Naca-Tn-3031-3040

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