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1

Physics Laboratory (U.S.). Optical Technology Division, red. Heat-flux sensor calibration. Gaithersburg, Md: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, Physics Laboratory, Optical Technology Division, 2004.

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2

A, Cyr M., Strange R. R i United States. National Aeronautics and Space Administration., red. Development of advanced high-temperature heat flux sensors. East Hartford, CT: United Technologies Corporation, Pratt & Whitney Group, Engineering Division, 1985.

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3

Mohammad, Aslam, i Langley Research Center, red. Diamond thin film temperature and heat-flux sensors. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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4

United States. National Aeronautics and Space Administration., red. Miniature high temperature plug-type heat flux guages. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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5

United States. National Aeronautics and Space Administration., red. Miniature high temperature plug-type heat flux guages. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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6

Paul, Kolodziej, i United States. National Aeronautics and Space Administration., red. Dual active surface heat flux gage probe. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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7

Paul, Kolodziej, i United States. National Aeronautics and Space Administration., red. Dual active surface heat flux gage probe. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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8

Yen, Yin-Chao. Sensible heat flux measurements near a cold surface. [Hanover, N.H.]: U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1995.

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9

Beddini, Robert A. Analysis of turbulent convective and radiative heat transfer in high temperature rocket chamber flows. New York: AIAA, 1987.

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10

Center, Langley Research, red. High temperature electromagnetic characterization of thermal protection system tile materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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11

Center, Langley Research, red. High temperature electromagnetic characterization of thermal protection system tile materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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12

Liebert, Curt H. Heat flux measurement in SSME turbine blade tester. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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13

A, Smith Eric, MacPherson J. Ian i United States. National Aeronautics and Space Administration., red. A comparison of surface sensible and latent heat fluxes for maircraft and surface measurements in FIFE 1987. [Washington, DC: National Aeronautics and Space Administration, 1990.

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14

E, Melis Matthew, i United States. National Aeronautics and Space Administration., red. A high heat flux experiment for verification of thermostructural analysis. [Washington, DC]: NASA, 1988.

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15

Vedova, B. Della. Geothermal heat flux at the COST B-2 and B-3 Wells, U.S. Atlantic continental margin. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1987.

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16

1945-, Mittal K. L., red. Polyimides and other high temperature polymers: Synthesis, characterization, and applications. Leiden: VSP, 2009.

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17

E, Melis Matthew, i United States. National Aeronautics and Space Administration., red. Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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18

1944-, Urban T. C., i Geological Survey (U.S.), red. Temperature, thermal-conductivity, and heat-flux data: Raft River area, Cassia County, Idaho (1974-1976). [Reston, Va.?]: Dept. of the Interior, U.S. Geological Survey, 1986.

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19

1944-, Urban T. C., i Geological Survey (U.S.), red. Temperature, thermal-conductivity, and heat-flux data: Raft River area, Cassia County, Idaho (1974-1976). [Reston, Va.?]: Dept. of the Interior, U.S. Geological Survey, 1986.

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20

Siegel, Robert. Two-flux and Green's function method for transient radiative transfer in a semitransparent layer. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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21

Siegel, Robert. Two-flux and Green's function method for transient radiative transfer in a semitransparent layer. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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22

Siegel, Robert. Two-flux and Green's function method for transient radiative transfer in a semitransparent layer. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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23

D, Craven P., Richards P. G i United States. National Aeronautics and Space Administration., red. A modified thermal conductivity for low density plasma magnetic flux tubes. [Washington, D.C: American Geophysical Union, 1995.

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24

D, Craven P., Richards P. G i United States. National Aeronautics and Space Administration., red. A modified thermal conductivity for low density plasma magnetic flux tubes. [Washington, D.C: American Geophysical Union, 1995.

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25

United States. National Aeronautics and Space Administration., red. Final report submitted to ... George C. Marshall Space Flight Center ... for NAS8-36955 D.O. 47 entitled high temperature materials characterization. Huntsville, Ala: Johnson Research Center, University of Alabama in Huntsville, 1990.

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26

1947-, Miller Robert A., i NASA Glenn Research Center, red. Thermal conductivity and elastic modulus evolution of thermal barrier coatings under high heat flux conditions. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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27

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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28

King, Paul I. Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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29

United States. National Aeronautics and Space Administration., red. Effect of NASA advanced designs on thermal behavior of Ni-H₂ cells. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

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30

Conference on Characterization and NDE of Heat Damage in Graphite Epoxy Composites (1993 Orlando, Fla.). Conference on Characterization and NDE of Heat Damage in Graphite Epoxy Composites: Proceedings, April 27-28, 1993, Orlando, Florida. Austin, Tex: Nondestructive Testing Information Analysis Center (NTIAC), Texas Research Institute Austin, 1993.

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31

United States. National Aeronautics and Space Administration., red. [FDNS code to predict wall heat fluxes or wall temperatures in rocket nozzles]: Final report. Huntsville, AL: University of Alabama in Huntsville, 1993.

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32

S, Zakany James, i United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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33

United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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34

S, Zakany James, i United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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35

B, Gurganus T., Walker J. A. 1939- i Langley Research Center, red. Development and characterization of powder metallurgy (PM) 2XXX series Al alloy products and metal matrix composite (MMC 2XXX Al/SiC materials for high temperature aircraft structural applications. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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36

United States. National Aeronautics and Space Administration., red. [An analysis of gamma ray burst time histories]: Final report. Huntsville, AL: University of Alabama in Huntsville, Summer Faculty Fellowship Research Continuation Program, 1994.

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37

1963-, Stephens Craig A., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Predicted thermal response of a cryogenic fuel tank exposed to simulated aerodynamic heating profiles with different cryogens and fill levels. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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38

R, Strange R., i United States. National Aeronautics and Space Administration., red. Development of sensors for ceramic components in advanced propulsion systems: Final report. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

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39

United States. National Oceanic and Atmospheric Administration., red. ATLAS OF SURFACE MARINE DATA 1994 VOLUME 6: HEAT FLUX SENSITIVITY TO SEA SURFACE TEMPERATURE... NOAA ATLAS NESDIS 12... U.S. DEPARTMENT OF COMMERCE... MARCH 1997. [S.l: s.n., 1998.

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40

S, Zakany James, i United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket heat transfer and combustion measurements. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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41

United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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42

S, Zakany James, i United States. National Aeronautics and Space Administration., red. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket combustion experiments. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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43

McLean, M. Physical and Elastic Characterization (Characterization of High-Temperature Materials, Vol 4). Ashgate Publishing, 1989.

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44

Mittal, K. L. Polyimides And Other High Temperature Polymers: Synthesis, Characterization. V.S.P. Intl Science, 2005.

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45

Muhamad, Nauman Malik. Inverse Estimation of Heat Flux and Temperature in 3D Finite Domain. Grin Verlag, 2016.

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46

Mechanical Testing (Characterization of High-Temperature Materials, Vol 3). Ashgate Publishing, 1988.

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47

National Aeronautics and Space Administration (NASA) Staff. Microsample Characterization of Coatings for Grcop-84 for High Heat Flux Applications. Independently Published, 2018.

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48

Mittal, K. L. Polyimides and Other High Temperature Polymers: Synthesis, Characterization and Applications. Taylor & Francis Group, 2007.

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49

Mittal, K. L. Polyimides and Other High Temperature Polymers: Synthesis, Characterization and Applications. Brill Academic Publishers, 2001.

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50

Polyimides and Other High Temperature Polymers: Synthesis, Characterization and Applications. Brill Academic Publishers, 2003.

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