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Books on the topic 'Film thickness'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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1

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

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2

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

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3

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Dynamic response of film thickness in spiral-groove face seals. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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4

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

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5

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

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6

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

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7

United States. National Aeronautics and Space Administration., ed. Enhancement of thickness uniformity of thin films grown by pulsed laser deposition. National Aeronautics and Space Administration, 1995.

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8

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

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9

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

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10

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

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11

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

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12

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

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13

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

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14

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

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15

E, Brewe David, Prahl Joseph M, United States. National Aeronautics and Space Administration., Lewis Research Center, and United States. Army Aviation Research and Technology Activity. Propulsion Directorate., eds. On the numerical solution of the dynamically loaded hydrodynamic lubrication of the point contact problem. National Aeronautics and Space Administration, 1990.

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16

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

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17

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

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18

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

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19

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

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20

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

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21

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

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22

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

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23

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

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24

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

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25

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

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26

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

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27

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

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28

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

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29

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

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30

United States. National Aeronautics and Space Administration., ed. High resolution video monitoring of coating thickness during plasma spraying. National Aeronautics and Space Administration, 1989.

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31

W, McConley Marc, and United States. National Aeronautics and Space Administration., eds. Stability of thin liquid sheet flows. National Aeronautics and Space Administration, 1997.

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32

J, Hamrock Bernard, and United States. National Aeronautics and Space Administration., eds. Fast approach for calculating film thicknesses and pressures in elastohydrodynamically lubricated contacts at high loads. National Aeronautics and Space Administration, 1985.

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33

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

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34

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

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35

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

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36

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

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37

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

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38

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

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39

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

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40

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

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41

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

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42

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

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43

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

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44

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

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45

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

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46

Perilloux, Bruce E. Thin-Film Design: Modulated Thickness and Other Stopband Design Methods. SPIE, 2002.

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47

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

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48

Currently Used Procedures for Dry Film Thickness Measurement and Recording for Coatings on Railcars. AMPP, 2022. https://doi.org/10.5006/ampp_tr21499-2022.

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Scope This AMPP technical report is intended for use by North America-based rail car manufacturers, owners, operators, and repairers who are seeking guidance concerning DFT measurement of coatings applied to rail cars. Rationale The procedures currently being used to measure and record the DFT of coatings on railcars are usually company-specific procedures that often vary drastically from one company to another. In some cases, these procedures are formal written documents that are used by the applicator or inspector while taking and recording DFT readings. In other cases, there are no formal w

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49

Enhancement of thickness uniformity of thin films grown by pulsed laser deposition. National Aeronautics and Space Administration, 1995.

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50

Holiday Detection of Internal Tubular Coatings of 250 to 760 μm (10 to 30 mils) Dry Film Thickness. AMPP, 1994. https://doi.org/10.5006/nace_tm0186-1994.

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Scope This NACE standard test method was prepared as a guide for evaluating the application of polymeric coatings of 250 to 760 (10 to 30 mils) to the internal surfaces of metallic tubular goods used in the oil and gas industry. It is not intended as a means of predicting the service life or service performance of these coatings. This test method is based on the current technology and experience of the petroleum production industry. NACE Standard TM0384 addresses holiday detection of internal tubular coatings of less than 250 (10 mils) dry film thickness. This NACE standard was originally prep

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