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1

Hahne, David E. Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration. Langley Research Center, 1989.

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2

Chan, K. B. Static and dynamic compression tests of filament-wound CFRP and GRP tubes under axial compression. UMIST, 1992.

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3

Riggle, Peter. Investigation of axial positioning for flexural compressors: Final technical report. Tri-Cities University Center, University of Washington, 1991.

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4

T, Armer G. S., and O'Dell T, eds. Fire, static, and dynamic tests of building structures: Proceedings of the Second Cardington Conference, Cardington, England, 12-14 March 1996. E & FN Spon, 1997.

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5

Collins, J. Scott. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. Langley Research Center, 1990.

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6

Schuster, D. M. Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel. National Aeronautics and Space Administration, Langley Research Center, 2001.

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7

Lee, Hosin David. Validation of the mix design process for cold in-place rehabilitation using foamed asphalt. Public Policy Center, University of Iowa, 2007.

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8

Whittenberger, J. Daniel. Mechanical properties of pure nickel alloys after long term exposures to LiOH and vacuum at 775 K. NASA, 1990.

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9

Armer, G. s. t. Fire, Static and Dynamic Tests of Building Structures. Taylor & Francis, 1997.

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10

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. National Aeronautics and Space Administration, Ames Research Center, 1989.

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11

Static tensile and tensile creep testing of five ceramic fibers at elevated temperatures: Final report. Composite Materials Research Group, Dept. of Mechanical Engineering, University of Wyoming, 1988.

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12

F, Harrington, and United States. National Aeronautics and Space Administration., eds. Static test induced loads verification beyond elastic limit. National Aeronautics and Space Administration, 1996.

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13

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. NASA Ames Research Center, 1989.

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14

Static tensile and tensile creep testing of four boron nitride coated ceramic fibers at elevated temperatures: Final report. NASA Ames Research Center, 1989.

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15

United States. National Aeronautics and Space Administration, ed. Study of static and dynamic stress effects in nonlinear solids: Semi-annual progress report, December 15, 1984-June 15, 1985. College of William and Mary, 1985.

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16

United States. National Aeronautics and Space Administration., ed. Study of static and dynamic stress effects in nonlinear solids: Semi-annual progress report, December 15, 1984-June 15, 1985. College of William and Mary, 1985.

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17

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

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18

R, Johnson Eric, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Dept., and Langley Research Center, eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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19

Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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20

R, Johnson Eric, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Dept., and Langley Research Center, eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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21

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

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22

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

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23

Center, Langley Research, ed. Analysis of wind tunnel oscillatory data of the X-31A aircraft. National Aeronautics and Space Administration, Langley Research Center, 1999.

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24

Mechanical properties of pure nickel alloys after long term exposures to LiOH and vacuum at 775 K. NASA, 1990.

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25

Waldmann, Carl, Neil Soni, and Andrew Rhodes. Respiratory monitoring. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780199229581.003.0006.

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Pulmonary function tests in critical illness 90End-tidal CO2 monitoring 92Pulse oximetry 94Pulmonary function test results in critically ill patients can be important prognostically and guide ventilatory and weaning strategies. However, they are not straightforward to measure in mechanically ventilated patients and remain limited to dynamic volumes. Fortunately, most modern mechanical ventilators are able to calculate and display static and dynamic lung volumes, together with derived values for airway resistance, compliance and flow/volume/time curves. The ability to monitor these changes afte
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