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1

L, Window A., ed. Strain gauge technology. 2nd ed. London: Elsevier Applied Science, 1992.

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2

E, Reed S., Hannah R. L, and Society for Experimental Mechanics, eds. Strain gauge users' handbook. London: Chapman & Hall, 1992.

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3

Valis, Tomas. Fiber optic Fabry-Perot strain gauge. [S.l.]: [s.n.], 1990.

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4

Harvey, J. F. A microprocessor controlled strain gauge calibration module. Melbourne, Victoria: Aeronautical Research Laboratory, 1989.

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5

S, Tripp John, Tcheng Ping, and Langley Research Center, eds. First International Symposium on Strain Gauge Balances. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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6

United States. National Aeronautics and Space Administration., ed. Two-dimensional surface strain measurement based on a variation of Yamaguchi's laser-speckle strain gauge. [Washington, D.C.]: NASA, 1990.

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7

United States. National Aeronautics and Space Administration., ed. Two-dimensional surface strain measurement based on a variation of Yamaguchi's laser-speckle strain gauge. [Washington, D.C.]: NASA, 1990.

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8

United States. National Aeronautics and Space Administration., ed. Two-dimensional surface strain measurement based on a variation of Yamaguchi's laser-speckle strain gauge. [Washington, D.C.]: NASA, 1990.

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9

United States. National Aeronautics and Space Administration., ed. Two-dimensional surface strain measurement based on a variation of Yamaguchi's laser-speckle strain gauge. [Washington, D.C.]: NASA, 1990.

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10

Pollock, N. An improved strain gauge transducer amplifier for wind tunnel use. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

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11

Law, R. D. Strain-gauge balance performance and internal temperature gradients measured in a cryogenic environment. London: HMSO, 1992.

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12

Baljeu, J. F. Development of a multi-component internal strain-gauge balance for model tests in a cryogenic wind tunnel. Amsterdam: National Aerospace Laboratory, 1988.

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13

United States. National Aeronautics and Space Administration, ed. FIRST INTERNATIONAL SYMPOSIUM ON STRAIN GAUGE BALANCES... NASA/CP-1999-209101/PT 2... OCT. 5, 1999. [S.l: s.n., 2000.

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14

United States. National Aeronautics and Space Administration, ed. First International Symposium On Strain Gauge Balances... NASA/CP-1999-209101/PT.1... July 9, 1999. [S.l: s.n., 1999.

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15

Chung, R. M. Development of an NBS polymer gage for dynamic soil stress measurement. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1985.

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16

P, Wnuk S., Wnuk V. P, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High temperature capacitive strain gage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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17

Lei, Jih-Fen. High temperature strain measurement with a resistance strain gage. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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18

Richards, W. Lance. A new correction technique for strain-gage measurements acquired in transient-temperature environments. Edwards, Calif: NASA Dryden Flight Research Center, 1996.

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19

Institution, British Standards. Calibration of bonded electrical resistance strain gauges. London: BSI, 1988.

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20

Oswald, Fred B. Gear tooth stress meaurements on the UH-60A helicopter transmission. Cleveland, Ohio: Lewis Research Center, 1987.

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21

United States. National Aeronautics and Space Administration., ed. High temperature static strain gage development contract. East Hartford, Conn: United Technologies Research Center, 1987.

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22

United States. National Aeronautics and Space Administration., ed. The apparent strain stability and repeatability of a BCL3 resistance strain gage. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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23

Staff, Measurements Group Technical, ed. Strain gage based transducers: Their design and construction. Raleigh, N.C., USA: The Group, 1988.

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24

United States. National Aeronautics and Space Administration., ed. High temperature static strain gage development: Final report. East Hartford, Conn: United Technologies Research Center, 1990.

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25

Murray, William M. The bonded electrical resistance strain gage: An introduction. New York: Oxford University Press, 1992.

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26

C, Greer L., Oberle Lawrence G, and United States. National Aeronautics and Space Administration., eds. Evaluation of Pd-Cr wires for strain gage application. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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27

C, Greer L., Oberle L. G, and United States. National Aeronautics and Space Administration., eds. Evaluation of Pd-Cr wires for strain gage application. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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28

C, Greer L., Oberle Lawrence G, and United States. National Aeronautics and Space Administration., eds. Evaluation of Pd-Cr wires for strain gage application. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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29

S, Bailey R., Lemkey F. D, and United States. National Aeronautics and Space Administration., eds. High temperature static strain gage alloy development: Final report. [East Hartford, Conn.]: United Technologies Research Center, 1987.

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30

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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31

Inc, Sverdrup Technology, and Lewis Research Center, eds. A resistance strain gage with repeatable and cancellable apparent strain for use to 800⁰ C. Brook Park, Ohio: Sverdrup Technology, inc., 1990.

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32

Anderson, W. L. High temperature strain gage technology for hypersonic aircraft development applications. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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33

F, Brinson H., Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Virginia Polytechnic Institute and State University, eds. Resistance fail strain gage technology as applied to composite materials. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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34

Kindermann, M. R. A slow strain-rate tensile testing machine. Melbourne, Victoria: Dept. of Defence, Aeronautical Research Laboratory, 1989.

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35

Patrick, Thollard, and Golvin Jean-Claude, eds. La Gaule retrouvée: Voyage avec Strabon. [Paris]: Errance, 2011.

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36

Lei, Jih-Fen. Development and characterization of PdCr temperature-compensated wire resistance strain gage. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Reserch Center, 1989.

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37

Valis, Tomas. Localized and distributed fiber-optic strain sensors embedded in composite materials. [Downsview, Ont.]: University of Toronto, 1991.

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38

Valis, Tomas. Localized and distributed fiber-optic strain sensors embedded in composite materials. [Downsview, Ont.]: Institute for Aerospace Studies, University of Toronto, 1992.

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39

C, Thompson Randolph, and Dryden Flight Research Facility, eds. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1991.

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40

C, Thompson Randolph, and Dryden Flight Research Facility, eds. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1991.

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41

Center, Langley Research, ed. Cryogenic strain gage techniques used in force balance design for the National Transonic Facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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42

C, Moore Thomas. Recommended strain gage application procedures for various Langley Research Center balances and test articles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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43

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Strain gage selection in loads equations using a genetic algorithm: Sigurd A. Nelson II. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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44

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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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

P, Boyden Richmond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Aerodynamic measurements and thermal tests of a strain-gage balance in a cryogenic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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47

Eckstrom, Clinton V. Loads calibrations of strain gage bridges on the DAST project aeroelastic research wing (ARW-2). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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48

Melle, Serge Michel. A wavelength demodulation system for use with fibre optic Bragg grating sensors. [Toronto, Ont.]: University of Toronto, 1992.

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49

Jenkins, Jerald M. A summary of numerous strain-gage load calibrations on aircraft wings and tails in a technology format. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1997.

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50

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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