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EFFECT OF A AFTERBODY GEOMETRY AND STING DIAMETER ON THE AERODYNAMIC CHARACTERISTICS OF SELENDER BODIES AT MACH NUMBERS FROM 1.57 TO 2.86.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 27.DDC classification: NASA | TN D-2042

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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-2042 (Browse shelf)	Not for loan		TR11945

Total holds: 0

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Previous	NASA TN D-2039 DIFUSSION STUDIES OF SEVERAL OXIDATION RESISTANT COATINGS ON M0-05TI MOLYBDENUM ALLOY AT 2.5000 DEGREE F.	NASA TN D-204 EXPERIMENTAL DETERMINATION OF THE TEMPERATURE AND DYNAMIC-STRAIN ENVIRONMENT OF A TUBULAR COMBUSTOR LINEAR IN A TURBOJET ENGINE	NASA TN D-2040 STUDY OD SEVERAL OXIDATION-RESISTANT COATINGS ON MO-0.51 ALLOY SHEET AT 2,5000 DEGREE F.	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 .	Next

Bound With Nasa Tn D-2041, 2043-50

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