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THERMAL-EXPANSION METHOD FOR LINING TANTALUM ALLOY TURBING WITH TUNGSTEN

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BookPublisher: Nasa, Washington, D.C. 1973Description: 23.DDC classification: NASA | TN D-7426 -

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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-7426 - (Browse shelf)	Not for loan		TR7649

Total holds: 0

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Previous	NASA TN D-7422 MULTIPLE REGRESSION TECHNIQUE FOR PTH DEGREE POLYNOMIALS WITH AND WITHOUT LINEAR CROSS PRODUCTS	NASA TN D-7423 EFFECTS OF NUCLEAR RADIATION ON A HIGH-RELIABILITY SILICON POWER DIODE	NASA TN D-7424 APPLICATION OF BOUNDARY INTEGRAL METHOD TO ELASTIC ANALYSIS OF V-NOTCHED BEAMS	NASA TN D-7426 - THERMAL-EXPANSION METHOD FOR LINING TANTALUM ALLOY TURBING WITH TUNGSTEN	NASA TN D-7427 - HYPERSONIC AERODYNAMIC CHARACTERISTICS OF A FAMILY OF POWER-LAW, WING-BODY CONFIGURATIONS	NASA TN D-7428 - LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 17-PERCENT-THICK AIRFOIL SECTION DESIGNED FOR GENERAL AVIATION APPLICATIONS	NASA TN D-7430 - HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS FOR LAMINAR SEPARATED FLOWS DOWNSTREAM OF REARWARD-FACING STEPS WITH AND WITHOUT MASS SUCTION	Next

Bound With Nasa Tn D-7425-30

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