Kapitel

LITERATURVERZEICHNIS
[65] Lumley, J. L. Computational modelling of turbulent flows. Adv. Appl. Mech. 18:
123–176. 1978.
[66] Lund, T. S. und Novikov, E. A. Parametrization of subgrid–scale stress by the
velocity gradient tensor. Annual Research Briefs of the Center for Turbulence
Research: 27–43. 1992.
[67] Lyn, D. A., Einav, S., Rodi, W. und Park, J. H. A laser-dopler velocimetry
study of ensemble-averaged characteristics of the turbulent near wake of a square
cylinder. J. Fluid. Mech. 304: 285–319. 1995.
[68] Menter, F. R. Influence of freestream values on k−ω turbulence model prediction.
AIAA Journal 30 (6): 1657–1659. 1992.
[69] Menter, F. R. Zonal two equation k−ω turbulence models for aerodynamic flows.
AIAA Paper 93–2906, American Inst. of Aeronautics and Astronautics. 1993.
[70] Menter, F. R. Two–equation eddy–viscosity turbulence models for engineering
applications. AIAA Journal 32 (8): 1598–1605. 1994.
[71] Morkovin, S. N. Effects of compressibility on turbulent flows. Mechanique de la
turbulence CNRS (ed.: A. Favre), Gordon Breach: 367–380. 1964.
[72] Neuzgliadov, V. G. Dokl. Akad. Nauk. 26: 238–386. 1960.
[73] Oberlack, M. Similarity in non–rotating and rotating turbulent pipe flows. J.
Fluid Mech. 379: 1–22. 1999.
[74] Obi, S., Perić, M. und Scheuerer, G. Second moment calculation procedure for
turbulent flows with colocated variable arrangement. AIAA Journal 29 (4): 585–
590. 1991.
[75] Ölcmen, S. M. und Simpson, R. L. Perspective: On the near wall similarity of
three-dimensional turbulent boundary layers. ASME Journal of Fluids Engineering
114: 487–495. 1992.
[76] Orlandi, P. und Fatica, M. Direct simulations of turbulent flow in a pipe rotating
about its axis. J. Fluid Mech. 343: 43–72. 1997.
[77] Peng, S. H., Davidson, L. und Holmberg, S. A modified low-Reynolds number
k − ω model for recirculating flows. ASME Journal of Fluids Engineering 119:
867–875. 1997.
[78] Pfuderer, D. G., Eifert, C. und Janicka, J. Nonlinear second moment closure
consistent with shear and strain flows. AIAA J. 35: 825–831. 1997.
[79] Piziali, R. A. An experimental investigation of 2d and 3d oscillating wing aerodynamics
for a range of angle of attack including stall. NASA Technical Memorandum
4632, NASA. 1993.
[80] Pope, S. B. A more general effective viscosity hypothesis. J. Fluid Mech. 72:
331–340. 1975.
206