Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

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2601. NACA research memorandum RM (series). E54E13. Effect of unequal air-flow distribution from twin inlet ducts on performance of axial-flow turbojet engine; by Curtis L. Walker, Joseph N. Sivo, and Emmert T. Jansen

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

2602. NACA research memorandum RM (series). E54F17. Investigation of high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment: 2, Performance of VorteX turbine at various stator settings [with list of references]: by Thomas R. Heaton, Donald E. Holeski, and Robert E. Forrette.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

2603. NACA research memorandum RM (series). E54E20. Effect of wedge-type boundary-layer diverters on performance of halfconical side inlets at Mach number 2.96 [with list of references]; by Harry W. Johnson and Thomas G. Piercy.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

2604. NACA research memorandum RM (series). E54F04. Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics: 3, Effect of turbine stator adjustment [with list of references]: by Harold E. Rohlik and John J. Reheske.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

2605. Research memorandum RM (series). E54E19. Effects of additives on corrosion and mass transfer in sodium hydroxidenickel systems under free-convection conditions; [with list of references]; by Americo F. Forestieri.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

2606. Research memorandum RM (series). E54F10. Preliminary investigation of stress-rupture and tensile strength of thermenol, an iron-aluminum alloy [with list of references]; by Charles A. Gyorgak.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

2607. Technical memorandum. 1365. Papers on shimmy and rolling behavior of landing gears presented at Stuttgart conference Oct. 16 and 17, 1941 [with lists of references]; translation [by Mary L. Mahler and others].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1954
SuDoc number:: Y 3.N 21/5:8/1365

2608. Technical notes. 3197. Mechanical properties at room temperature of 4 cermets of titanium carbide with nickel binder [with list of references]; by Aldie E. Johnson, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1954
SuDoc number:: Y 3.N 21/5:6/(nos.)

2609. Technical notes. 3206. Torsional vibrations of hollow thin-walled cylindrical beams [with list of references]; by Edwin T. Kruszewski and Eldon E. Kordes.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1954
SuDoc number:: Y 3.N 21/5:6/(nos.)

2610. Technical notes. 3212. Nonlinear theory of bending and buckling of thin elastic shallow spherical shells [with list of references]; by A. Kaplan and Y. C. Fung.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1954
SuDoc number:: Y 3.N 21/5:6/(nos.)

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