26.12.2012 Views

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

”cell”, containing this solution <strong>and</strong> 50mm long by 15mm high by 155mm wide, was placed in a superconducting magnet at Marshall<br />

Space Flight Center. The magnetic field was measured at various positions within the bore of the magnet using a Hall effect<br />

probe. In this way, a position was found where the magnetic field gradient was predominantly upward; the magnitude of the gradient<br />

could then be adjusted by adjusting the current of the magnet. The ends of the cell consisted of machined copper blocks maintained<br />

at controlled temperatures by circulating water from constant temperature baths. The walls of the cell were of rectangular<br />

section glass tubing so that the cell contents could be seen. Velocities arising from thermal gradients within the cell were measured<br />

by particle image velocimetry (PIV). Particles used for this purpose were silver-coated hollow glass spheres of micrometers diameter<br />

<strong>and</strong> nearly the same density as the solution. A central vertical plane of the cell was illuminated by a laser beam passing through<br />

a cylindrical lens. Digital images of the particles were captured on a CCD camera <strong>and</strong> fed to a computer so that frame-to-frame<br />

movements of particles traveling with the fluid were captured. These images were employed to compute velocity maps using commercial<br />

PIV software. In a typical experiment the cold end of the cell was maintained at 10C <strong>and</strong> the warm end at 30 C. With no<br />

current in the magnet, i.e.- with natural -convection allowed to occur, the fluid was observed to circulate with an average speed<br />

of approximately 0.3 millimeters per second. It was visually apparent that this circulation was diminished as the current was<br />

increased. At currents of approximately 20A the flow was halted, to within the precision of the PIV measurements. At yet higher<br />

currents the convection was reversed with the hotter solution sinking <strong>and</strong> the cooler solution rising. At 40A this reversed convection<br />

had speeds averaging 0.43 millimeters per second. The measurements of susceptibility <strong>and</strong> density allow an estimate of the<br />

field gradient necessary to halt convection in the experiment. That estimate was 7.8T (squared) per meter <strong>and</strong> the convection was<br />

observed to halt in the magnet at a current giving 7.21T (squared) per meter from the magnetic field measurements. Calculations<br />

of the flow have been carried out using the computational fluid dynamics software FLUENT <strong>and</strong> show good agreement with the<br />

measurements.<br />

Author<br />

Convection; Magnetic Permeability; Solidification; Temperature Dependence; Computational Fluid Dynamics<br />

50<br />

26<br />

METALS AND METALLIC MATERIALS<br />

�������� ��������� ��������� ��� ���������� ���������� �� ������ ��� �������� ���������� ��� �����������<br />

<strong>2000</strong>0061970 NASA Glenn Research Center, Clevel<strong>and</strong>, OH USA<br />

Bithermal Low-Cycle Fatigue Evaluation of Automotive Exhaust System Alloy SS409<br />

Lu, Gui-Ying, Arvin Exhaust Systems, USA; Behling, Mike B., Arvin Exhaust Systems, USA; Halford, Gary R., NASA Glenn<br />

Research Center, USA; [<strong>2000</strong>]; 32p; In English, 1 Nov. 1999, Cincinnati, OH, USA; Sponsored by American Society for Metals,<br />

USA; No Copyright; Avail: CASI; A03, Hardcopy; A01, Microfiche<br />

This investigation provides, for the first time, cyclic strainrange-controlled, thermomechanical fatigue results for the ferritic stainless<br />

steel alloy SS409. The alloy has seen extensive application for automotive exhaust system components. The data were generated to calibrate<br />

the Total Strain Version of the Strainrange Partitioning (TS-SRP) method for eventual application to the design <strong>and</strong> durability assessment<br />

of automotive exhaust systems. The thermomechanical cyclic lifetime <strong>and</strong> cyclic stress-strain constitutive behavior for alloy SS409 were<br />

measured using bithermal tests cycling between isothermal extremes of 400 <strong>and</strong> 800 C. Lives ranged up to 10,000 cycles to failure with<br />

hold-times of 0.33 to 2.0 minutes. The bithermal fatigue behavior is compared to isothermal, strain-controlled fatigue behavior at both 400<br />

<strong>and</strong> 800 C. Thermomechanical cycling was found to have a profound detrimental influence on the fatigue failure resistance of SS409<br />

compared to isothermal cycling. Supplementary bithermal cyclic stress-strain constitutive tests with hold-times ranging from 40 seconds<br />

up to 1.5 hours were conducted to calibrate the TS-SRP equation for extrapolation to longer lifetime predictions. Observed thermomechanical<br />

(bithermal) fatigue lives correlated well with lives calculated using the calibrated TS-SRP equations: 70% of the bithermal fatigue data<br />

fall within a factor of 1.2 of calculated life; 85% within a factor of 1.4; <strong>and</strong> 100% within a factor of 1.8.<br />

Author<br />

Cycles; Fatigue Life; Fatigue (Materials); Alloys; Ferritic Stainless Steels; Stress-Strain Relationships<br />

<strong>2000</strong>0064082 United Engineering Foundation, Inc., New York, NY USA<br />

An Interdisciplinary Approach to the Science of Alloys in Metals, Minerals <strong>and</strong> Other Materials Systems, 7 Jan. 1999 -<br />

6 Mar. <strong>2000</strong><br />

Gonis, A.; Melke, A.; Rajan, K.; Turchi, P. E.; Sep. 15, 1999; 19p; In English; 2nd; Alloy, 8-13 Aug. 1999, Davos, Switzerl<strong>and</strong><br />

Contract(s)/Grant(s): N00014-99-1-0895<br />

Report No.(s): AD-A368788; 99-BS; No Copyright; Avail: CASI; A01, Microfiche; A03, Hardcopy; Abstract Only; Abstract<br />

Only

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!