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1

L, Window A., red. Strain gauge technology. Wyd. 2. London: Elsevier Applied Science, 1992.

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2

E, Reed S., Hannah R. L i Society for Experimental Mechanics, red. 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 i Langley Research Center, red. 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., red. 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., red. 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., red. 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., red. 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, red. 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, red. 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 i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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., red. 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., red. 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, red. 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., red. 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 i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. 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 i United States. National Aeronautics and Space Administration., red. 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, i Lewis Research Center, red. 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 i Virginia Polytechnic Institute and State University, red. 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, i Golvin Jean-Claude, red. 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, i Dryden Flight Research Facility, red. 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, i Dryden Flight Research Facility, red. 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, red. 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., red. 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 i Langley Research Center, red. 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 i Langley Research Center, red. 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, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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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