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THE FLOW ABOUT A SECTION OF A FINITE-ASPECT-RATIO NACA 0015 AIRFOIL ON A TRANSONIC BUMP

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BookSeries: National Advisory Committee For Aeronautics-Tn-3036. Publisher: Naca, Washington 1953Description: 30.DDC classification: TR | NACA-3036

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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-3036 (Browse shelf)	Not for loan		TR3538

Total holds: 0

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Previous	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	TR NACA-3035 A PRCLIMINARY STUDY OF THE PROBLEM OF DESIGNING HIGH-SPEED AIRPLANES WITH SATISFACTORY INHERENT DAMPING OF THE DUTCH SOLL OSCILLATION	TR NACA-3036 THE FLOW ABOUT A SECTION OF A FINITE-ASPECT-RATIO NACA 0015 AIRFOIL ON A TRANSONIC BUMP	TR NACA-3038 LOW-SPEED DRAG OF CYLINDERS OF VARIOUS SHAPES	TR NACA-3039 EXPERIMENTAL STRESS ANALYSIS OF STIFFENED CYLINDERS WITH COTOUTS	TR NACA-3040 USE OF TWO-DIMENSIONAL DATA IN ESTIMATING LOADS ON A 45 % SWEPTBACK WIND WITH SLATS AND PARTIAL -SPAN FLAPS	Next

Bound With: Naca-Tn-3031-3040

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