论文信息 - Numerical Investigation of the Flow Angularity Effects of the NASA Langley UPWT on the Ares I DAC1 0.01-Scale Model

Numerical Investigation of the Flow Angularity Effects of the NASA Langley UPWT on the Ares I DAC1 0.01-Scale Model

Investigation of the non-uniform ow angularity e ects on the Ares I DAC-1 in the Langley Unitary Plan Wind Tunnel are explored through simulations by OVERFLOW. Veri cation of the wind tunnel results are needed to ensure that the standard wind tunnel calibration procedures for large models are valid. The expectation is that the systematic error can be quanti ed, and thus be used to correct the wind tunnel data. The corrected wind tunnel data can thenn be used to quantify the CFD uncertainties.

Henry C. Lee | Goetz Klopfer | Jeff T. Onufer

[1] T. Barth,et al. A one-equation turbulence transport model for high Reynolds number wall-bounded flows , 1990 .

[2] John R. Micol. Langley Research Center's Unitary Plan Wind Tunnel: Testing Capabilities and Recent Modernization Activities , 2001 .

[3] Dochan Kwak,et al. The Overgrid Interface for Computational Simulations on Overset Grids , 2002 .

[4] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[5] Michael J. Aftosmis,et al. Adjoint Error Estimation and Adaptive Refinement for Embedded-Boundary Cartesian Meshes , 2007 .

[6] Robert H. Nichols,et al. Solver and Turbulence Model Upgrades to OVERFLOW 2 for Unsteady and High-Speed Applications , 2006 .

[7] W. J. Monta,et al. Description and calibration of the Langley unitary plan wind tunnel , 1981 .