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BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01

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BookPublisher: Nasa, Washington, D.C. 1963Description: 40.DDC classification: NASA | TN D-2048

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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-2048 (Browse shelf)	Not for loan		TR11951

Total holds: 0

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Previous	NASA TN D-2045 RESIDUAL STATIC STRENGTH OF SEVERAL TITANIUM AND STAINLESS-STEEL ALLOYS AND ONE SUPERALLOYS AT-109 DEGREE F, 70 DEGREE F, AND 550 DEGREE F .	NASA TN D-2046 JET EFFECTS AT SUPERSONIC SPEEDS ON BASE AND AFTERBODY PRESSURES OF A MISSILE MODEL HAVING SINGLE AND MULTIPLE JETS.	NASA TN D-2047 EFFECTS OF DIFFERENTIAL PRESSURE, THARMAL STRESS, AND BUCKLING ON FLUTTER OF FLAT PANELS WITH LENGHT-WIDTH RATIO OF 2	NASA TN D-2048 BOUNDARY-LAYER VELOCITY PROFILES AND SKIN FRICTION DUE TO SURFACE ROUGHNESS ON AN OGIVE CYLINDER AT MACH NUMBERS OF 1.61 AND 2.01	NASA TN D-2049 FEASIBILITY STUDY OF A BANG-BANG PATH CONTROL FOR A REENTRY VEHICLE.	NASA TN D-205 FREE-FLIGHT INVESTIGATION AT MACH NUMBERS BETWEEN 0.5 AND 1.7 OF THE ZERO-LIFT ROLLING EFFECTIVENESS AND DRAG OF VARIOUS SURFACE, SPOILER, AND JET CONTROLS ON AN 80(DEGRE) DELTA-WING MISSILE	NASA TN D-2050 EFFECTS OF FLANK LOSSES IN THE THEORY OF SPACE-PROBE ENTRY UNDER CONDITIONS OF HIGH MASS LOSS.	Next

Bound With Nasa Tn D-2041-47, 2049-50

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