Książki na temat „Film thickness”

Perilloux, Bruce. Thin-film design: Modulated thickness and other stopband design methods. Bellingham, WA: SPIE Press, 2002.

Thin-film design: Modulated thickness and other stopband design methods. Bellingham, WA: SPIE Press, 2002.

Olechowski, Mark Joseph. Analysis of single and multi-grade lubricant film thickness in a diesel engine. Springfield, Va: Available from the National Technical Information Service, 1990.

National Association of Corrosion Engineers. Holiday detection of internal tubular coatings of less than 250um (10mils) dry film thickness. Houston: NACE, 1994.

Ingles, Edward N. Instrumentation of a diesel engine for oil film thickness measurement using fiber optics and laser fluorescence. Springfield, Va: Available from the National Technical Information Service, 1991.

National Association of Corrosion Engineers. Holiday detection of internal tubular coatings of less than 10 mils (0.25 mm) dry film thickness. Houston: NACE, 1989.

Ingles, Edward N. Instrumentation of a diesel engine for oil film thickness measurement using fiber optics and laser fluorescence. Springfield, Va: Available from the National Technical Information Service, 1991.

National Association of Corrosion Engineers. Holiday detection of internal tubular coatings of 10 to 30 mils(0.25to 0.76 mm) dry film thickness. Houston: NACE, 1989.

United States. National Aeronautics and Space Administration., red. System for the growth of bulk SiC crystals by modified CVD techniques: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

W, McConley Marc, i United States. National Aeronautics and Space Administration., red. Stability of thin liquid sheet flows. [Washington, DC: National Aeronautics and Space Administration, 1997.

Hartman, Richard M. Tritium method oil consumption and its relation to oil film thicknesses in a production diesel engine. Springfield, Virginia: Available from the National Technical Information Service, 1990.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M. (5338 Montgomery Blvd., NE, Suite 400, Albuquerque, 87109-1311): U.S. Geological Survey, 2002.

Heywood, Charles E. Estimation of alluvial-fill thickness in the Mimbres ground-water basin, New Mexico, from interpretation of isostatic residual gravity anomalies. Albuquerque, N.M: U.S. Dept. of the Interior, U.S. Geological Survey, 2002.

Jacob, Sarkis Y. Systematic studies of the effect of pressure on magnetic and electronic properties of La2/3Ca1/3MnO3 thin films with various thicknesses. St. Catharines, Ont: Brock University, Dept. of Physics, 1999.

The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

1935-, Aboudi Jacob, Arnold S. M i NASA Glenn Research Center, red. The effect of interface roughness and oxide film thickness on the inelastic response of thermal barrier coatings to thermal cycling. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

National Aeronautics and Space Administration (NASA) Staff. Minimum Film Thickness in Elliptical Contacts for Different Regimes of Fluid-Film Lubrication. Independently Published, 2018.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Dynamic response of film thickness in spiral-groove face seals. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Perilloux, Bruce E. Thin-Film Design: Modulated Thickness and Other Stopband Design Methods. SPIE, 2002. http://dx.doi.org/10.1117/3.453202.

National Aeronautics and Space Administration (NASA) Staff. On the Correlation of Specific Film Thickness and Gear Pitting Life. Independently Published, 2019.

Center, Goddard Space Flight, red. Evaluation of a procedure for the measurement of thin film thickness by X-ray reflectivity. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1997.

United States. National Aeronautics and Space Administration., red. Enhancement of thickness uniformity of thin films grown by pulsed laser deposition. [Washington, D.C.?: National Aeronautics and Space Administration, 1995.

Enhancement of thickness uniformity of thin films grown by pulsed laser deposition. [Washington, D.C.?: National Aeronautics and Space Administration, 1995.

National Association of Corrosion Engineers., red. Holiday detection of internal tubular coatings less than 250 um(10 mils) dry-film thickness. Houston: NACE, 2002.

S, Cheng H., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., red. A computer solution for the dynamic load, lubricant film thickness and surface temperatures in spiral bevel gears. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Oil film thickness measurement and analysis for an angular contact ball bearing operating in parched elastohydrodynamic lubrication. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

ICE-ACCRETION SCALING USING WATER-FILM THICKNESS PARAMETERS... NASA/CR--2003-211826... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION... JUNE. [S.l: s.n., 2003.

United States. National Aeronautics and Space Administration., red. ICE-ACCRETION SCALING USING WATER-FILM THICKNESS PARAMETERS... NASA/CR--2003-211826... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION... JUNE. [S.l: s.n., 2003.

National Association of Corrosion Engineers., red. Holiday detection of internal tubular coatings of 250 to 760 um (10 to 30 mils) dry-film thickness. Houston: NACE, 2002.

United States. National Aeronautics and Space Administration., red. ICE-ACCRETION SCALING USING WATER-FILM THICKNESS PARAMETERS... NASA/CR--2003-211826... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION... JUNE. [S.l: s.n., 2003.

E, Brewe David, Prahl Joseph M, United States. National Aeronautics and Space Administration., Lewis Research Center i United States. Army Aviation Research and Technology Activity. Propulsion Directorate., red. On the numerical solution of the dynamically loaded hydrodynamic lubrication of the point contact problem. [Washington, D.C.?]: National Aeronautics and Space Administration, 1990.

National Aeronautics and Space Administration (NASA) Staff. Effect of Interface Roughness and Oxide Film Thickness on the Inelastic Response of Thermal Barrier Coatings to Thermal Cycling. Independently Published, 2018.

M, Thompson Peter, i NASA Glenn Research Center, red. The effect of sliding speed on film thickness and pressure supporting ability of a point contact under zero entrainment velocity conditions. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2000.

M, Thompson Peter, i NASA Glenn Research Center, red. The effect of sliding speed on film thickness and pressure supporting ability of a point contact under zero entrainment velocity conditions. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2000.

J, Bachmann Klaus, i United States. National Aeronautics and Space Administration., red. P-polarized reflectance spectroscopy: A high sensitive real-time monitoring technique to study surface kinetics under steady state epitaxial deposition conditions. [Washington, D.C: National Aeronautics and Space Administration, 1995.

J, Bachmann Klaus, i United States. National Aeronautics and Space Administration., red. P-polarized reflectance spectroscopy: A high sensitive real-time monitoring technique to study surface kinetics under steady state epitaxial deposition conditions. [Washington, D.C: National Aeronautics and Space Administration, 1995.

J, Bachmann Klaus, i United States. National Aeronautics and Space Administration., red. P-polarized reflectance spectroscopy: A high sensitive real-time monitoring technique to study surface kinetics under steady state epitaxial deposition conditions. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Netzer, Falko P., i Claudine Noguera. Oxide Thin Films and Nanostructures. Oxford University Press, 2021. http://dx.doi.org/10.1093/oso/9780198834618.001.0001.

United States. National Aeronautics and Space Administration., red. Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1996 - 16 June 1997. [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., red. Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1997 - 16 June 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1996 - 16 June 1997. [Washington, DC: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., red. Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1997 - 16 June 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

United States. National Aeronautics and Space Administration., red. Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1997 - 16 June 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

United States. National Aeronautics and Space Administration., red. Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1996 - 16 June 1997. [Washington, DC: National Aeronautics and Space Administration, 1997.

Non-coalescence effects in microgravity: (NAG 3-1894), performance report for the period 17 June 1997 - 16 June 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.