PKK Library Search for 'au:"JOHNSTON,JAMES R"'

OXIDATION AND THERMAL FATIGUE CRACKING OF NICKEL-AND COBALT-BASE ALLOYS IN A HIGH VELOCITY GAS STREAM

By Johnston,James R. Nasa, Washington, D.C. 1969 . 48 , Bound With Nasa Tn D-5371-80

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NASA Technical Note [NASA TN D-5273]: Effect of temperature and pressure on cavitation damage to a cobalt base alloy in sodium

Washington NASA 1969 . 19p , Bound together NASA TN D-5271 to 5280 | Bound vol. Acc. No. 101151 contains Acc. No. TR7891 to TR7899

Place Hold on NASA Technical Note [NASA TN D-5273]: Effect of temperature and pressure on cavitation damage to a cobalt base alloy in sodium

EFFECT OF CYCLIC CONDITIONS ON THE DYNAMIC OXIDATION OF GAS TURBINE SUPERALLOYS

By Johnston,James R. Nasa, Washington, D.C. 1974 . 21 , Bound With Nasa Tn D-7611-19

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PERFORMANCE OF TWO BARON -MODIFIED S-816 ALLOYS IN A TURBOJET OPERATED AT 1650 DEGREE F

By Waters,Willam J,Signorelli,Robert A. Nasa,Washington, D.C. 1959 . 30 , Bound With Nasa Memo2-3-59e,3-4-59e-3-18-59e.Lack No-3-7-59e-3-8-59e,3-11-59e-3-16-59e

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EXEPERIMENTAL EVALUATION OF CERMET TURBINE STATOR BLADES FOR USE AT ELEVATED GAS TEMPERATURES.

By Chiarito,Patrick T. Nasa, Washington, D.C. 1959 . 25 , Bound With: Nasa Memo 2-5-59e-2-12-59e,2-14-59e-2-27-59e.Lack No-Nasa Memo 2-7-59e,2-8-59e,2-10-59e,2-12-59e,2-14-59e-2-16-59e,2-18-59e-2-19-59e,2-21-59e-2-22-59e,2-24-59e,2-26-59e.

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EFFECT OF COVER GAS PRESSURES ON ACCELERATED CAVITATION DAMAGE IN SODIUM.

By Young,Stanley G. Nasa, Washington, D.C. . 23 , Bound With Nasa Tn D-4231-34, 4236-40

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OXIDATION AND THERMAL FATIGUE OF COATED AND UNCOATED NX-188 NICKEL-BASE ALLOY IN A HIGH-VELOCITY GAS STREAM

By Johnston,James R. Nasa, Washington, D.C. 1972 . 39 , Bound With Nasa Tn D-6780-6794,6796-6799

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NASA Technical Note [NASA TN D-3426]: Accelerated cavitation damage of steels and superalloys in liquid metals

Washington NASA 1966 . 34p , Bound together NASA TN D-3421 to 3430 | Bound vol. Acc. No. 64323 contains Acc. No. TR15546 to TR15554

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NASA Technical Note [NASA TN D-3428]: Performance of rocket nozzle materials with several solid propellants

Washington NASA 1966 . 25p , Bound together NASA TN D-3421 to 3430 | Bound vol. Acc. No. 64323 contains Acc. No. TR15546 to TR15554

Place Hold on NASA Technical Note [NASA TN D-3428]: Performance of rocket nozzle materials with several solid propellants

HOT-SALT STRESS-CORROSION OF A TITANIUM ALLOY UNDER A SIMULATED TURBINE-ENGINE COMPRESSOR ENVIRONMENT

By GRAY,HUGH R. NASA, WASHINGTON, D.C. 1969 . ,35,,,,,, , Bound with NASA TN D-5511-5518

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Engine Operating Conditions That Cause Thermal - Fatigue Cracks In Turbojet - Engine Buckets

By Johnston, James. R. Washington National Aeronautics And Space Administration 1959 . various paging

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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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Oxidation and thermal fatigue cracking of nickel and cobalt base alloys in a high velocity gas stream [NASA TN D-5376]

By Johnston, James R.. Washington, D. C. National Aeronautics and Space Administration 1969 . 48p , Bound vol. contains NASA TN D 5371-5380

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