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1

Dahotre, Narendra B., Janet M. Hampikian e John E. Morral, eds. Elevated Temperature Coatings. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2001. http://dx.doi.org/10.1002/9781118787694.

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2

Orange, Thomas W. Elevated temperature crack propagation. [Washington, DC: National Aeronautics and Space Administration, 1993.

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3

United States. National Aeronautics and Space Administration, ed. Elevated temperature biaxial fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1985.

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4

Orange, Thomas W. Elevated temperature crack propogation. [Washington, DC: National Aeronautics and Space Administration, 1993.

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5

H, Van Stone R., e United States. National Aeronautics and Space Administration., eds. Elevated temperature crack growth: Final report. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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6

N, Malik S., e United States. National Aeronautics and Space Administration, eds. Elevated temperature crack growth: Annual report. Cincinnati, Ohio: General Electric, Aircraft Engine Business Group, Advanced Technology Programs Dept., 1987.

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7

1947-, Yau Jen-Fu, e United States. National Aeronautics and Space Administration, eds. Elevated temperature crack growth: Annual report. Cincinnati, Ohio: General Electric, Aircraft Engine Business Group, Advanced Technology Programs Dept., 1985.

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8

Piascik, RS, RP Gangloff e A. Saxena, eds. Elevated Temperature Effects on Fatigue and Fracture. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1997. http://dx.doi.org/10.1520/stp1297-eb.

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9

Healy, Joseph Cornelius. Short fatigue crack growth at elevated temperature. Birmingham: Universityof Birmingham, 1989.

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10

C, Watkins J., Nitzel M. E e U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., eds. Performance of MOV stem lubricants at elevated temperature. Washington, DC: Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 2001.

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11

Ratkovich, John. Processing and elevated temperature ductility of Aluminum alloy 7475. Monterey, Calif: Naval Postgraduate School, 1989.

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12

Sreeramesh, Kalluri, United States. Army Aviation Research and Technology Activity. e United States. National Aeronautics and Space Administration., eds. Elevated temperature axial and torsional fatigue behavior of Haynes 188. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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13

J, Zamzow M., Shanks D. E e Reno Research Center (United States. Bureau of Mines), eds. Pretreatment of bauxite with oxygen or air at elevated temperature. Reno, NV: U.S. Dept. of the Interior, Bureau of Mines, Reno Research Center, 1990.

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14

J, Carino Nicholas, e National Institute of Standards and Technology (U.S.), eds. Mechanical properties of high-strength concrete at elevated temperatures. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2001.

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15

J, Carino Nicholas, e National Institute of Standards and Technology (U.S.), eds. Mechanical properties of high-strength concrete at elevated temperatures. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2001.

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16

J, Carino Nicholas, e National Institute of Standards and Technology (U.S.), eds. Mechanical properties of high-strength concrete at elevated temperatures. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2001.

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17

Hall, A. M. Summary report on elevated temperature tests for asbestos-free gasket materials. [Houston? Tex.]: National Association of Corrosion Engineers, 1990.

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18

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Automated measurement of crack length and loadline displacement at elevated temperature. S.l: s.n, 1988.

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19

Cissel, Matthew B. Elevated temperature properties of a dispersion strengthened Al-[Fe, V, Si] alloy. Monterey, Calif: Naval Postgraduate School, 1991.

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20

A, Salem Jonathan, Seshadri Srinivasa G e United States. National Aeronautics and Space Administration., eds. Fracture resistance of a TiB?□particle/SiC matrix composite at elevated temperature. Washington, D.C: National Aeronautics and Space Administration, 1988.

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21

1960-, Salem J. A., e United States. National Aeronautics and Space Administration., eds. Elevated temperature mechanical behavior of monolithic and SiC whisker-reinforced silicon nitrides. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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22

Hua, Xiang. Processing and Properties of Encapsulated van der Waals Materials at Elevated Temperature. [New York, N.Y.?]: [publisher not identified], 2022.

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23

Whittenberger, J. Daniel. Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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24

van, Leeuwen H. P., e Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting,, eds. Automated measurement of crack length and load line displacement at elevated temperature. Neuilly sur Seine: Agard, 1988.

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25

Center, Langley Research, ed. Effects of elevated temperature on the viscoplastic modeling of graphite/polymeric composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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26

Leeuwen, H. P. van. Automated measurement of crack length and load line displacement at elevated temperature. Neuilly sur Seine, France: AGARD, 1988.

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27

Crapo, Chuck. Salmon quality: The effects of elevated refrigerated seawater chilling temperatures. Fairbanks: Alaska Sea Grant College Program, University of Alaska, 1987.

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28

Kostiainen, Katri. Wood properties of northern forest trees grown under elevated CO₂, O₃ and temperature. Helsinki: Finnish Society of Forest Science, 2007.

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29

Jornaz, Mustapha Isa. The Mechanics of the drawing of polygonal sections from round at elevated temperature. Birmingham: AstonUniversity Department of Mechanical & Production Engineering, 1991.

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30

1935-, Adams Donald Frederick, e United States. National Aeronautics and Space Administration., eds. Static tensile and tensile creep testing of five ceramic fibers at elevated temperatures. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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31

Andriesse, C. D. Fission product source term: Chemical form and release of fission products at elevated temperature. Luxembourg: Commission of the European Communities, 1986.

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32

Hodkinson, Victoria. The effect of waveshape on fatigue crack growth in nickel superalloys at elevated temperature. Portsmouth: University of Portsmouth, Dept. of Mechanical and Manufacturing Engineering, 1997.

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33

Center, Lewis Research, ed. Modfications of system for elevated temperature testing and stress-strain measurement of metal matrix composites. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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34

Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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35

Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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36

P, Bansal Narottam, Gyekenyesi John P e NASA Glenn Research Center, eds. Dependency of shear strength on test rate in SiC/BSAS ceramic matrix composite at elevated temperature. [Cleveland, Ohio: NASA Glenn Research Center, 2003.

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37

Choi, Sung Rak. Dependency of shear strength on test rate in SiC/BSAS ceramic matrix composite at elevated temperature. [Cleveland, Ohio: NASA Glenn Research Center, 2003.

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38

David, Nathenson, Prakash Vikas e NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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39

David, Nathenson, Prakash Vikas e NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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40

R, Kennedy J., e Langley Research Center, eds. Superplastic forming and diffusion bonding of rapidly solidified, dispersion strengthened aluminum alloys for elevated temperature structural applications. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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41

Reardon, Lawrence F. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. Moffett Field, Calif: Ames Research Center, 1989.

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42

Morison, William Donald. The effects of moisture loss and elevated temperature upon the material damping of fibre reinforced polymer matrix composites. Downsview, Ont: Institute for Aerospace Studies, 1988.

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43

Morison, William Donald. The effects of moisture loss and elevated temperature upon the material damping of fibre reinforced polymer matrix composites. [Downsview, Ont.]: [Institute for Aerospace Studies], 1987.

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44

Schauder, Thomas J. The effects of thermomechanical processing parameters on elevated temperature behavior of a 6061 Al-Al2O3 metal matrix composite. Monterey, Calif: Naval Postgraduate School, 1992.

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45

Kevin, Rivers H., Smith Russell W e Langley Research Center, eds. Thermal output of WK-type strain gauges on various materials at cryogenic and elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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46

Kevin, Rivers H., Smith Russell W e Langley Research Center, eds. Thermal output of WK-type strain gauges on various materials at cryogenic and elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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47

Branch, M. C. Ignition and combustion of bulk metals at normal, elevated, and reduced gravity: Annual technical report, NASA grant no. NAG-3-1685. Boulder, CO: Center for Combustion Research, University of Colorado at Boulder, 1995.

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48

F, Adams Donald, Zimmerman Richard S e Ames Research Center, eds. Static tensile and tensile creep testing of four boron nitride coated ceramic fibers at elevated temperatures: Final report. Moffett Field, Calif: NASA Ames Research Center, 1989.

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49

Schmidt, Carl. Changes in optical reflectance and pigmentation of the coral Montastraea faveolata in response to elevated temperature and ultraviolet radiation. Bellingham, WA: Huxley College of Environmental Studies, Western Washington University, 1999.

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50

Elevated temperature biaxial fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1985.

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