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1

Dahotre, Narendra B., Janet M. Hampikian, and 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., and 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., and 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, and 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, and 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, and 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., and 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, and 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, and 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, and 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, and 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, and 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., and 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., and 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, and 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, and 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, and 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, and 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., and 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, and 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, and 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, and 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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