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1

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

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2

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

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3

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

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4

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

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5

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

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6

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

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7

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

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8

American Institute of Aeronautics and As. Recommended Practice: Calibration of Subsonic and Transonic Wind Tunnels. AIAA (American Institute of Aeronautics & Ast, 2004.

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9

American Institute of Aeronautics and As. Recommended Practice: Calibration of Subsonic and Transonic Wind Tunnels (Aiaa Standards). AIAA (American Institute of Aeronautics & Ast, 2003.

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10

American Institute of Aeronautics and As. Recommended Practice: Calibration and Use of Internal Strain-Gage Balances With Application to Wind Tunnel Testing (AIAA Standards). AIAA (American Institute of Aeronautics & Ast, 2004.

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11

American Institute of Aeronautics and As. Recommended Practice: Calibration and Use of Internal Strain Gage Balances With Application to Wind Tunnel Testing (Aiaa Standards). AIAA (American Institute of Aeronautics & Ast, 2003.

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12

As, American Institute of Aeronautics and. Recommended Practice: Wind Tunnel Testing. AIAA (American Institute of Aeronautics & Ast, 2003.

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13

As, American Institute of Aeronautics and. Recommended Practice: Wind Tunnel Testing. AIAA (American Institute of Aeronautics & Ast, 2004.

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14

American Institute of Aeronautics and As. Recommended Practice: Terminology for Unmanned Aerial Vehicles and Remotely Operated Aircraft. AIAA (American Institute of Aeronautics & Ast, 2004.

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15

American Institute of Aeronautics and As. Recommended Practice: The Cfd General Notation System--Standard Interface Data Structures. AIAA (American Institute of Aeronautics & Ast, 2002.

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16

American Institute of Aeronautics and As. Recommended Practice: Wind Tunnel Testing; Practitioners Volume. AIAA (American Institute of Aeronautics & Ast, 2003.

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17

Magee, Patrick, and Mark Tooley. Measurement and monitoring in anaesthesia. Edited by Antony R. Wilkes and Jonathan G. Hardman. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780199642045.003.0025.

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Abstract:
This chapter introduces some basic physical principles that contribute to the function of various monitors used in anaesthetic practice. Topics include biological signal processing, operational amplifiers, including single-ended amplifiers, and the benefit of patient-isolated differential amplifiers; it includes filtering, digital processing, and electrodes. The generic principles of transducers are introduced, including resistive, capacitive, and inductance strain gauges used in transducers, photoelectric, piezoelectric, and chemical transducers, calibration of transducers, and the significance of resonance and damping in measurement systems. Since both are widely used in monitoring systems, there is an introduction to spectroscopy and magnetism.
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18

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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19

Strain gage selection in loads equations using a genetic algorithm: Sigurd A. Nelson II. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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20

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

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21

Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020). American Institute of Aeronautics and Astronautics, Inc., 2020. http://dx.doi.org/10.2514/4.106019.

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22

Recommended Practice: Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091-2003). American Institute of Aeronautics and Astronautics, Inc., 2003. http://dx.doi.org/10.2514/4.476464.

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23

United States. National Aeronautics and Space Administration., ed. A SUMMARY OF NUMEROUS STRAIN-GAGE LOAD CALIBRATIONS ON AIRCRAFT WINGS AND TAILS IN A TECHNOLOGICAL FORMAT... NASA-TM-4804... OCT. 20, 1997. s.n., 1998.

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