PKK Library Search for 'au:"Waters, William J. "'

NICKEL BASE ALLOY, WAZ-20, WITH IMPROVED STRENGTH IN THE 2000(DEGREE) F RANGE

By Waters,William J. Nasa, Washington, D.C. 1969 . 22 , Bound With Nasa Tn D-5341-60

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EXPLORATORY INVESTIGATION OF ADVANCED-TEMPERATURE NICKEL-BASE ALLOYS

By Freche,John C. Nasa, Washington, D.C. 1959 . 39 , Bound With Nasa Memo 4-9-59e-4-30-59e

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EVALUATION OF TWO NICKEL-BASE ALLOYS, ALLOY 713C AND NASA TAZ-8A, PRODUCED BY EXTRUSION OF PREALLOYED POWDERS

By Freche,John C,Waters,William J. Nasa, Washington, D.C. 1969 . 31 , Bound With Nasa Tn D-5241-5247,5249-5250

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APPLICATION OF DIRECTIONAL SOLIDIFICATION TO A NASA NICKEL-BASE ALLOY (TAZ-8B)

By Freche,John C,Waters,William J. Nasa, Washington, D.C. 1968 . 21 , Bound With Nasa Tn D-4381-89

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A NICKEL-BASE ALLOY, NASA WAZ-16 WITH POTENTIAL FOR GAS TURBINE STATOR VANE APPLICATION

By WATERS,WILLIAM J. NASA, WASHINGTON, D.C. 1974 . ,24,,,,,, , Bound with NASA TN D-7649-7660

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A Nickel base alloy waz 20, with improved strength in the 2000 degree to 2200 degree F range [NASA TN D-5352]

By Waters, William J.. Washington,D.C. National Aeronautics and Space Administration 1969 . 22p

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Investigation of Columbium-Modified NASA Taz-8 Superalloy

By Waters, William J.. Washington, D. C. National Aeronautics and Space Administration (NASA) 1966 . 30

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NASA Technical Note [D271-280]

, NASA Technical Note D271: Analysis of Elastic-plastic stress distribution in thin-wall cylinders and spheres subjected to internal pressure and nuclear radiation heating/ by Donald F. Johnson | NASA Technical Note D272: Thermal-stress fatigue cracking of turbine buckets operated at 1700 degree F in a turbojet engine with long periods of operation between starts/ by Robert A. Signorelli, James R. Johnston and William J. Waters | NASA Technical Note D273: Numerical computation of aerodynamic heating of liquid propellants/by John L. Kramer, Herman H. Lowell and William H. Roudebush | NASA Technical Note D274: Crash-fire protection system for A J57 turbojet engine using water as a cooling and inerting agent/ by Dugald O. Black | NASA Technical Note D275: Compilation of thermodynamic properties, transport properties, and theoretical rocket performance of gaseous hydrogen/ by Charles R. King | NASA Technical Note D276: Performance study of a piston-type pump for liquid hydrogen/ by Arnold E. Biermann and William G. Shinko | NASA Technical Note D277: Application of various techniques for determining local heat-trasfer coefficients in a rocket engine from transient experimental data / by Curt H. Liebert, James E. Hatch, and Ronald W. Grant | NASA Technical Note D278: Free-flight observation of a separated turbulent flow including heat transfer up to mach 8.5 / by Dudley George McConnell | NASA Technical Note D279: Operational method of determining initial contour of and pressure field about a supersonic jet/ Gerald W. Englert | NASA Technical Note D280: Flight measurement of wall-pressure fluctuations and boundary-layer turbulence/ by Harold R. Mull and Joseph S. Algranti

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NASA MEMO 3-3-59E

By Waters, William J. . Washington National Aeronautics and Space Administration (NASA) 1959 . 30p , NASA MEMORANDUM 3-2-59E Bounded Volumes Accession No. 102446; Contents: TR7450-57

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