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RESIDUAL STATIC STRENGTH OF SEVERAL TITANIUM AND STAINLESS-STEEL ALLOYS AND ONE SUPERALLOYS AT-109 DEGREE F, 70 DEGREE F, AND 550 DEGREE F .

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BookPublisher: Nasa, Washington, D.C. 1963Description: 21.DDC classification: NASA | TN D-2045

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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-2045 (Browse shelf)	Not for loan		TR11948

Total holds: 0

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Previous	NASA TN D-2042 EFFECT OF A AFTERBODY GEOMETRY AND STING DIAMETER ON THE AERODYNAMIC CHARACTERISTICS OF SELENDER BODIES AT MACH NUMBERS FROM 1.57 TO 2.86.	NASA TN D-2043 CALCULATED RADIO ATTENUATION DUE TO PLASMA SHEAT ON HYPERSONIC BLUNT-NOSED CONE.	NASA TN D-2044 FREE-FLIGHT INVESTIGATION OF THE DEPLOYMENT OF A PARAWING RECOVERY DEVICE FOR A RADIO-CONTROLLED 1/5-SCALE DYNAMIC MODEL SPACECRAFT.	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	Next

Bound With Nasa Tn D-2041-44, 2046-50

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