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COMPARISON OF EXPERIMENTAL AND THEORETICAL RESULTS FOR THE COMPRESSIBLE TURBULENT-BOUNDARY-LAYER SKIN FRICTION WITH ZERO PRESSURE GRADIENT

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BookPublisher: Nasa, Washington, D.C. 1963Description: 55.DDC classification: NASA | TN D-1795 -

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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-1795 - (Browse shelf)	Not for loan		TR8666

Total holds: 0

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Previous	NASA TN D-1782 - SIMPLIFIED METHOD FOR MEASURING HUMAN TRANSFER FUNCTION	NASA TN D-1793 - CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UPTO 25(DEGREE)	NASA TN D-1794 - STUDY OF SEVERAL FACTORS AFFECTING THE FLUTTER CHARACTERISTICS CALCULATED FOR TWO SWEPT WINGS BY PISTON THEORY AND COMPARISON WITH EXPERIMENTS	NASA TN D-1795 - COMPARISON OF EXPERIMENTAL AND THEORETICAL RESULTS FOR THE COMPRESSIBLE TURBULENT-BOUNDARY-LAYER SKIN FRICTION WITH ZERO PRESSURE GRADIENT	NASA TN D-1803 INVESTIGATION OF THE EFFECTS OF VARIABLE-AMPLITUDE LOADINGS ON FATIGUE CRACK PROPGATION PATTERNS.	NASA TN D-1804 PERFORMANCE OF A PLUG NOZZLE HAVING A CONCAVE CENTRAL BASE WITH AND WITHOUT TERMINAL FAIRINGS AT TRANSONIC SPEEDS.	NASA TN D-1807 WIND-TUNNEL MEASUREMENT OF PROPELLER WHIRL-FLUTTER SPEEDS AND STATIC-STABILITY DERIVATIVES AND AOMPARISON WITH THEORY.	Next

Bound With Nasa Tn D-1791-95

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