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TURBULENT SKIN FRICTION AT HIGH MACH NUMBERS AND RENOLDS NUMBERS IN AIR AND HELIUM

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Material type: Text

TextPublication details: Nasa, Washington, D.C. 1961Description: 39DDC classification:

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TR R-82 (Browse shelf(Opens below))	Not for loan		TR14355

Total holds: 0

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Previous	NASA TR R-248 NEW ONE-STEP INTEGRATION METHODS OF HIGH-ORDER ACCURACY APPLIED TO SOME PROBLEMS IN CELESTIAL MECHANICS	NASA TR R-249 A STUDY OF DAMPING IN NONLINEAR OSCILLATIONS	NASA TR R-250 HYPERSONIC AERODYNAMIC PERFORMANCE OF MINIMUM-WAVE-DRAG BODIES	NASA TR R-82 TURBULENT SKIN FRICTION AT HIGH MACH NUMBERS AND RENOLDS NUMBERS IN AIR AND HELIUM	NASA TR R-83 A THEORETICAL STUDY OF THE ANGULAR MOTIONS OF SPINNING BODIES IN SPACE	NASA TR R-84 ORDINATES AND THEORETICAL PRESSURE-DISTRIBUTION DATA FOR NACA 6- AND 6A-SERIES AIRFOIL SECTIONS WITH THICKNESSES FROM 2 TO 21 AND FROM 2 TO 15 PERCENT CHORD, RESPECTIVELY	NASA TR R-85 A NONLINEAR THEORY FOR PREDICTING THE EFFECTS OF UNSTEADY LAMINAR, TURBULENT, OR TRANSITIONAL BOUNDARY LAYERS ON THE ATTENUATION OF SHOCK WAVES IN A SHOCK TUBE WITH EXPERIMENTAL COMPARISON	Next

Bound With Nasa Tr R-81,83-90

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