Sensitivity to Physical and Numerical Modeling in Navier-Stokes Simulations

Author:

Cella Ubaldo12,Rizzi Arthur12

Affiliation:

1. MSc Student, Aerosp. Dept., Politecnico di Milano, Italy.

2. Prof., Div. of Aerodyn., Dept. of Aeronautics, Royal Inst. of Technology, Stockholm, Sweden.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference13 articles.

1. Baldwin B. S. and Lomax H. (1978). “Thin layer approximation and algebraic model for separated turbulent flows.” AIAA Paper 78-257 American Institute of Aeronautics and Astronautics Reston Va.

2. Cella U. ( 1998). “Assessment of physical and numerical models in NSMB for flow around aerofoils and wings ” Master's thesis Royal Institute of Technology (KTH) Stockholm Sweden.

3. Gacherieu C. and Weber C. (1998). “Assessment of algebraic and one-equation turbulence models for the transonic turbulent flow around a full aircraft configuration.” AIAA Paper No. 98-2737 American Inst. of Aeronautics and Astronautics Reston Va.

4. McGhee R. J. and Beasley W. D. (1979). “Low-speed aerodynamic characteristics of a 13-percent-thick medium-speed airfoil designed for general aviation application.” Tech. Rep. NASA Langley Research Center Hampton Va.

5. Muller B. and Rizzi A. ( 1990). “Modelling of turbulent transonic flow around aerofoils and wings.” Applied numerical methods vol. 6 603–613.

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