Books on the topic 'High-stability'

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1

Bansal, Narottam P. Chemical stability of high-temperature superconductors. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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2

Taylor, Mark. A high performance spectral code for nonlinear MHD stability. [New York]: Courant Institute of Mathematical Sciences, New York University, 1992.

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3

Lovatt, M. G. The preparation and stability of high Tc ceramic superconductors. [S.l: The Author], 1994.

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4

Erdmann, Natalie. Identification of high-copy-number inhibitors of P1 plasmid stability. Ottawa: National Library of Canada, 1998.

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5

Junold, Helga Erika. The stability of block protection systems in high velocity flows. Salford: University of Salford, 1989.

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6

Mohler, Ronald R. Nonlinear stability and control study of highly maneuverable high performance aircraft. Corvallis, Ore: Oregon State University, Dept. of Electrical and Computer Engineering, 1991.

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7

Hossain, Jahangir, and Hemanshu Roy Pota. Robust Control for Grid Voltage Stability: High Penetration of Renewable Energy. Singapore: Springer Singapore, 2014. http://dx.doi.org/10.1007/978-981-287-116-9.

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8

Xu, Quanyun A. Stability-indicating HPLC methods for drug analysis. 3rd ed. Washington, D.C: American Pharmacists Association, 2008.

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9

Xu, Quanyun A. Stability-indicating HPLC methods for drug analysis. Washington, D.C: American Pharmaceutical Association, 1999.

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10

Johnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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11

Nunn, M. E. Evaluation of stone mastic asphalt (SMA): A high stability wearing course material. Crowthorne, Berks: Transport Research Laboratory, 1994.

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12

Johnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. [S.l.]: [s.n.], 1986.

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13

Lobo, M. Stability theorems concerning high order explicit algorithms for the linear advection equation. Cranfield, Eng: College of Aeronautics, Cranfield Institute of Technology, 1985.

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14

Joshi, Arunkumar G. The stability of wedge shaped blocks protection systems in high velocity flows. Salford: University of Salford, 1989.

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15

Papageorgiou, Demetrious T. The stability of two-dimensional wakes and shear-layers at high Mach numbers. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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16

Papageorgiou, D. T. The stability of two-dimensional wakes and shear-layers at high Mach numbers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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17

Ravi, Ramakrishnan. A computational examination of directional stability for smooth and chined forebodies at high-a. Hampton, Va: Langley Research Center, 1992.

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18

Yu, Wai Haung. Desferrioxamine analysis by high performance liquid chromatography, stability and metabolic inhibition by monoamine oxidase inhibitors. Ottawa: National Library of Canada, 1994.

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19

Mulkens, M. J. M. Steady-state experiments for measurements of aerodynamic stability derivatives of a high incidence research model using the College of Aeronautics Whirling Arm. Cranfield, Bedford, England: Cranfield Institute of Technology, College of Aeronautics, 1990.

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20

Smith, Ian Heaton. A study of foam stability and the kinetics of bubble growth in glass at high temperatures. Salford: University of Salford, 1987.

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21

Mohler, Ronald R. Phase 2 annual report on Nonlinear stability and control study of highly maneuverable high performance aircraft. Corvallis, Ore: Oregon State University, Dept. of Electrical and Computer Engineering, 1992.

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22

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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23

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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24

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1996.

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25

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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26

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. Washington, D.C: National Aeronautics and Space Administration, 1996.

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27

Stoel, Max van der. Peace and stability through human and minority rights: Speeches by the OSCE High Commissioner on National Minorities. Baden-Baden: Nomos, 1999.

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28

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1997.

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29

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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30

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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31

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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32

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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33

Streeck, Wolfgang. High equality,low activity: The contribution of the social welfare system to the stability of the German collective bargaining regime. Badia Fiesolana, San Domenico (FI): European University Institute, 2001.

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34

Svoboda, J. The effect of particle size and colloid stability on the wet high-intensity magnetic separation of uranium from cyanidation reisdues. Randburg, South Africa: Council for Mineral Technology, 1986.

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35

Streeck, Wolfgang. High equality, low activity: The contribution of the social welfare system to the stability of the German collective bargaining regime. San Domenico di Fiesole, Italy: European University Institute, Robert Schuman Centre, 2001.

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36

Jorden, Frank L. Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane. Hampton, Va: Langley Research Center, 1992.

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37

Connolly, J. C. Improving the reliability and modal stability of high power 870 nm AlGaAs CSP laser diodes for applications to free space communication systems. Hampton, Va: Langley Research Center, 1990.

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38

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

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39

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

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40

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

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41

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: NASA, Dryden Flight Research Center, 1997.

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42

D, Southwick Robert, Gallops George W, and United States. National Aeronautics and Space Administration., eds. High stability engine control (HISTEC). [Washington, DC]: National Aeronautics and Space Administration, 1996.

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43

(Editor), K. A. Dannemann, G. E. Fuchs (Editor), and T. C. Deragon (Editor), eds. Long Term Stability of High Temperature Materials. Minerals, Metals, & Materials Society, 1999.

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44

High stability engine control (HISTEC) flight test results. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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45

Strong stability preserving high-order time discretization methods. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2000.

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46

United States. National Aeronautics and Space Administration., ed. A high-temperature heat sensitive element. Washington, D.C: National Aeronautics and Space Administration, 1986.

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47

A high-temperature heat sensitive element. Washington, D.C: National Aeronautics and Space Administration, 1986.

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48

A high-temperature heat sensitive element. Washington, D.C: National Aeronautics and Space Administration, 1986.

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49

L, St Clair Terry, and Langley Research Center, eds. The mechanical stability of polyimide films at high pH. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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50

C, DeLaat John, and Lewis Research Center, eds. The high stability engine control (HISTEC) program: Flight demonstration phase. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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