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EXPERIMENTAL DETERMINATION OF THE TEMPERATURE AND DYNAMIC-STRAIN ENVIRONMENT OF A TUBULAR COMBUSTOR LINEAR IN A TURBOJET ENGINE

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BookPublisher: Nasa, Washington, D.C. 1960Description: 33.DDC classification: NASA | TN D-204

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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-204 (Browse shelf)	Not for loan		TR14833

Total holds: 0

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Previous	NASA TN D-2034 SUBSONIC AERODYNAMIC HEAT TRASFER TO A SURFACE RECESSED WITHIN A FORWARD STAGNATION REGION SLIT.	NASA TN D-2038 EXPERMENTAL AND CALCULATED RESULTS OF A FLUTTER INVESTIGATION OF SOME VERY LOW ASPECT-RATIO FLAT-PLATE SURFACE AT MACH NUMBERS FROM 0.62 TO 3.00	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.	Next

Bound With Nasa Tn D-201-203,205-210

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