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1

David, Hampton R., and Lewis Research Center, eds. The Microgravity Isolation Mount: A linearized state-space model á la Newton and Kane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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2

David, Hampton R., and Lewis Research Center, eds. The Microgravity Isolation Mount: A linearized state-space model á la Newton and Kane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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3

Lee, Myung W. Linearized inversion of reflection traveltimes. U.S. G.P.O., 1991.

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4

Chechelnitsky, Michael Y. Adaptive error estimation in linearized ocean general circulation models. Massachusetts Institute of Technology, 1999.

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5

M, Verdon Joseph, and United States. National Aeronautics and Space Administration., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

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6

M, Verdon Joseph, and United States. National Aeronautics and Space Administration., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

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7

Montgomery, Matthew D. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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8

C, Hall Kenneth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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9

Bosworth, John T. Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data. National Aeronautics and Space Administration, 1992.

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10

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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11

Stoliker, P. C. Linearized poststall aerodynamics and control law models of the X-31A aircraftn and comparison with flight data. National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

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12

M, Verdon Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows: Under contract NAS3-26618. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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13

Carroll, Chris. Death to the log-linearized consumption Euler equation!: (and very poor health to the second-order approximation). National Bureau of Economic Research, 1997.

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14

An analytically linearized helicopter model with improved modeling accuracy. Princeton University, Dept. of Mechanical and Aerospace Engineering, 1991.

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15

National Aeronautics and Space Administration (NASA) Staff. Glovebox Integrated Microgravity Isolation Technology: A Linearized State-Space Model. Independently Published, 2018.

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16

Succi, Sauro. Model Boltzmann Equations. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199592357.003.0008.

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This chapter deals with simplified models of the Boltzmann equation, aimed at reducing its mathematical complexity, while still retaining the most salient physical features. As observed many times in this book, the Boltzmann equation is all but an easy equation to solve. The situation surely improves by moving to its linearized version, but even then, a lot of painstaking labor is usually involved in deriving special solutions for the problem at hand. In order to ease this state of affairs, in the mid-fifties, stylized models of the Boltzmann equations were formulated, with the main intent of
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17

National Aeronautics and Space Administration (NASA) Staff. Microgravity Isolation Mount: A Linearized State-Space Model a la Newton and Kane. Independently Published, 2018.

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18

A reduced order model of the linearized incompressible Navier-Strokes equations for the sensor/actuator placement problem. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2000.

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19

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

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20

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. National Aeronautics and Space Administration, 1996.

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21

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows: Under contract NAS3-26618. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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22

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows: Under contract NAS3-26618. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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23

A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows: Under contract NAS3-26618. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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24

Morawetz, Klaus. Deep Impurities with Collision Delay. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198797241.003.0017.

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The linearised nonlocal kinetic equation is solved analytically for impurity scattering. The resulting response function provides the conductivity, plasma oscillation and Fermi momentum. It is found that virial corrections nearly compensate the wave-function renormalizations rendering the conductivity and plasma mode unchanged. Due to the appearance of the correlated density, the Luttinger theorem does not hold and the screening length is influenced. Explicit results are given for a typical semiconductor. Elastic scattering of electrons by impurities is the simplest but still very interesting
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25

Friedrich, Manuel. Effective Theories for Brittle Materials: A Derivation of Cleavage Laws and Linearized Griffith Energies from Atomistic and Continuum Nonlinear Models ... Zur Mathematik, Physik Und Informatik). Logos Verlag Berlin, 2015.

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