PKK Library Search for 'au:" Signorelli, Robert A."'

STRESS-RUPTURE PROPERTIES OF TUNGSTEN WIRE FROM 1200(DEGREE) TO 2500(DEGREE) F

By Mcdanels,David L. Nasa, Washington, D.C. 1966 . 20 , Bound With Nasa Tn D-3461-70

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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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FIBER-METAL COMPOSITE MATERIALS

By Weeton,John W. Nasa, Washington, D.C. 1966 . 41 , Bound With Nasa Tn D-3521-3529

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STRESS-RUPTURE AND TENSILE PROPERTIES OF REFRACTORY-METAL WIRES AT 2000(DEGRE) AND 2200(DEGRE) F(1093 DEGRE AND 1204 DEGRE C)

By Petrasek,Donald W. Nasa, Washington, D.C. 1969 . 39 , Bound With Nasa Tn D-5131-5138,5140-5150

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PRELIMINARY EVALUATION OF TUNGSTEN ALLOY FIBER - NICKEL-BASE ALLOY COMPOSITES FOR TURBOJET ENGINE APPLICATIONS

By Petrasek,Donald W. Nasa, Washington, D.C. 1970 . 27 , Bound With Nasa Tn D-5570-74,5576-79

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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

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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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