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1

Alexandris, Georgios. Supersonic flow past two oscillating airfoils. Monterey, Calif: Naval Postgraduate School, 1998.

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2

Gordon, David R. Computational unsteady flow dynamics: Oscillating flow about a circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

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3

Beyers, M. E. Flow-field interference produced by an asymmetrical support strut. Ottawa, Ont: National Research Council Canada, Institute for Aerospace Research, 1993.

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4

Lotshaw, John E. Numerical analysis of oscillating flow about a circular cylinder. Monterey, Calif: Naval Postgraduate School, 1992.

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5

Brydges, Bruce E. Flow visualization of dynamic stall on an oscillating airfoil. Monterey, Calif: Naval Postgraduate School, 1989.

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6

Coward, Adrian V. Stability of oscillatory two phase Couette flow. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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7

Kozel, Karel. Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil. Praha, Czechoslovakia: Information Centre for Aeronautics, 1986.

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8

Schippers, H. TULIPS: a method to calculate transonic potential flow about oscillating airfoils. Amsterdam, Netherlands: National Aerospace Laboratory, 1988.

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9

Srinivasan, G. R. Evaluation of turbulence models for unsteady flows of an oscillating airfoil. [New York]: Pergamon, 1995.

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10

Dadman, R. Flow around normal and yawed cylinders oscillating over a plane bed. Manchester: UMIST, 1996.

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11

Nakamichi, Jiro. Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing. Tokyo: National Aerospace Laboratory, 1988.

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12

Christopoulos, George P. Oscillating-flow wind tunnel studies for a circulation control circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

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13

Hall, Philip. On the instability of the flow in an oscillating tank of fluid. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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14

Drummond, Colin K. Mass transfer from a sphere in an oscillating flow with zero mean velocity. [Washington, D.C.]: NASA, 1990.

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15

Mirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.

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16

Balakumar, P. On the receptivity and non-parallel stability of traveling disturbances in rotating disk flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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17

Leonard, B. P. ULTRA-SHARP nonoscillatory convection schemes for high-speed steady multidimensional flow. [Washington, D.C.]: NASA, 1990.

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18

Obayashi, Shigeru. Navier-Stokes computations on full wing-body configuration with oscillating control surfaces. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

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19

Obayashi, Shigeru. Navier-Stokes computations on full wing-body configuration with oscillating control surfaces. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

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20

Obayashi, Shigeru. Navier-Stokes computations on full wing-body configuration with oscillating control surfaces. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

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21

Obayashi, Shigeru. Navier-Stokes computations on full wing-body configuration with oscillating control surfaces. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

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22

Obayashi, Shigeru. Extension of a streamwise upwind algorithm to a moving grid system. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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23

Obayashi, Shigeru. Extension of a streamwise upwind algorithm to a moving grid system. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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24

Gaster, Michael. The velocity field created by a shallow bump in a boundary layer. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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25

Gaster, Michael. The velocity field created by a shallow bump in a boundary layer. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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26

Neace, Kerry S. A computational and experimental investigation of the propulsive and lifting characteristics of oscillating airfoils and airfoil combinations in incompressible flow. Monterey, Calif: Naval Postgraduate School, 1992.

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27

Cahill, Thomas A. Visualization of the flow field around an oscillating model of the USS Enterprise (CVN-65) in a simulated atmospheric boundary layer. Monterey, California: Naval Postgraduate School, 1988.

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28

Cirovic, Srdjan. Characterizing flow-induced oscillation in a mechanical trachea. Ottawa: National Library of Canada, 1996.

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29

Sarpkaya, Turgut. In-line and transverse forces on smooth and rough cylinders in oscillatory flow at high Reynolds numbers. Monterey, Calif: Naval Postgraduate School, 1986.

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30

Streitlien, Knut. Extracting energy from unsteady flows through vortex control. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1994.

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31

Amin, Norsarahaida. Oscillation-induced mean flows and heat transfer. Norwich: University of East Anglia, 1989.

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32

Johnson, Anthony William. Steady and oscillating internal tube flows using a vortex method. Manchester: University of Manchester, 1995.

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33

A, Stepani͡a︡nt͡s︡ I͡U︡, ed. Propagation of waves in shear flows. Singapore: World Scientific, 1998.

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34

Fransson, T. Numerical investigation of unsteady subsonic compressible flows through an oscillating cascade. Lausanne: EPFL, 1986.

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35

Davies, D. E. Modification and use of an Euler program for calculating flows about harmonically oscillating aerofoils. London: HMSO, 1990.

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36

Supersonic Flow Past Two Oscillating Airfoils. Storming Media, 1998.

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37

United States. National Aeronautics and Space Administration., ed. Numerical analysis of flow through oscillating cascade sections. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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38

United States. National Aeronautics and Space Administration., ed. Oscillating-flow regenerator test rig: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

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39

United States. National Aeronautics and Space Administration., ed. Oscillating-flow regenerator test rig: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

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40

United States. National Aeronautics and Space Administration., ed. Oscillating-flow regenerator test rig: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

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41

McCoy, William T. Stability of the vortex motion in oscillating flow. 1986.

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42

United States. National Aeronautics and Space Administration., ed. Cascades with harmonically oscillating blades in supersonic flow. Washington, DC: National Aeronautics and Space Administration, 1988.

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43

Sanford, Fleeter y United States. National Aeronautics and Space Administration., eds. Aerodynamics of a linear oscillating cascade. [Washington, DC: National Aeronautics and Space Administration, 1990.

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44

Center, Langley Research, ed. Artificial boundary conditions for computation of oscillating external flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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45

Pressure wave propagation studies for oscillating cascades. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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46

Unsteady-flow-field predic[t]ions for oscillating cascades. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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47

United States. National Aeronautics and Space Administration., ed. Unsteady-flow-field predic[t]ions for oscillating cascades. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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48

R, Reddy T. S. y United States. National Aeronautics and Space Administration., eds. Numerical simulations of supersonic flow through oscillating cascade sections. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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49

Description of an oscillating flow pressure drop test rig. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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50

Description of an oscillating flow pressure drop test rig. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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