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THERMAL ELECTROMOTIVE FORCE CHANGE FOR SOME NOBLE AND REFRACTORY-METAL THERMOCOUPLES AT 1600 K IN VACUUM, AIR, AND ARGON.

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BookPublisher: Nasa, Washington, D.C. 1970Description: 33.DDC classification: NASA | TN D-7027

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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-7027 (Browse shelf)	Not for loan		TR11118

Total holds: 0

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Previous	NASA TN D-7024 CARBON MONOXIDE OXIDATION RATES COMPUTED FOR AUTOMOBILE EXHAUST MANIFOLD REACTOR CONDITIONS.	NASA TN D-7025 ELECTRON RADIATION EFFECTS IN RUBY.	NASA TN D-7026 DIGITAL COMPUTER PROGRAM FOR ANALYSIS OF CHUGGING INSTABILITIES.	NASA TN D-7027 THERMAL ELECTROMOTIVE FORCE CHANGE FOR SOME NOBLE AND REFRACTORY-METAL THERMOCOUPLES AT 1600 K IN VACUUM, AIR, AND ARGON.	NASA TN D-7028 VALIDATION OF THE GAS GENERATOR METHOD OF CALCULATING JET-ENGINE THRUST AND EVALUATION OF XB-70-1 AIRPLANE ENGINE PERFORMANCE AT GROUND STATIC CONDITIONS.	NASA TN D-703 SEASONAL, LATITUDINAL AND DIURNAL VARIATIONS IN THE UPPER ATMOSPHERE	NASA TN D-7031 - AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE MODEL WITH A LIFT FAN MOUNTED IN A 5-PERCENT-THICK TRIANGULAR WING,INCLUDING THE EFFECTS OF BLC ON THE LIFT-FAN INLET3	Next

Bound With Nasa Tn D-7020-26, 7028.

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