Abstract. Unstructured mesh drag prediction is discussed using a drag decomposition method. This method decomposes total drag into wave, profile, induced and spurious drag components, the latter resulting from numerical diffusion and errors. Computational results show that the method reliably predicts drag and is capable of meaningful drag decomposition. The accuracy of drag prediction is increased by eliminating the spurious drag component from the total drag. It is also confirmed that the physical drag components are almost independent of the mesh resolution or scheme modification
SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-AERO--2146) / BLDSC -...
The drag prediction workshop series (DPW), held over the last six years, and sponsored by the AIAA A...
The goal of this thesis is to improve the wave drag estimation techniques in the aircraft conceptual...
Unstructured mesh drag prediction is discussed using a drag decomposition method. This method decomp...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140615/1/1.c032622.pd
The 3rd AIAA Drag Prediction Workshop (DPW 3) showed a wide range of predictions using unstructured ...
In this report the contribution of the National Aerospace Laboratory NLR to the ’CFD Drag Pre- dicti...
This paper describes the theoretical development and implementation issues of a far field induced dr...
This paper reviews the importance of numerical drag prediction in an aircraft design environment. A ...
SIGLEAvailable from British Library Document Supply Centre- DSC:D37692/81 / BLDSC - British Library ...
In the aerodynamic shape design, the drag prediction has always been an extremely challenging missio...
Preliminary design or feasibility study is the first stage13; of an aircraft design during which the...
The prediction and decomposition of drag associated to Propulsive System Integration (PSI) is invest...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143019/1/6.2017-0960.pd
Preliminary design or feasibility study is the first stage13; of an aircraft design during which the...
SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-AERO--2146) / BLDSC -...
The drag prediction workshop series (DPW), held over the last six years, and sponsored by the AIAA A...
The goal of this thesis is to improve the wave drag estimation techniques in the aircraft conceptual...
Unstructured mesh drag prediction is discussed using a drag decomposition method. This method decomp...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140615/1/1.c032622.pd
The 3rd AIAA Drag Prediction Workshop (DPW 3) showed a wide range of predictions using unstructured ...
In this report the contribution of the National Aerospace Laboratory NLR to the ’CFD Drag Pre- dicti...
This paper describes the theoretical development and implementation issues of a far field induced dr...
This paper reviews the importance of numerical drag prediction in an aircraft design environment. A ...
SIGLEAvailable from British Library Document Supply Centre- DSC:D37692/81 / BLDSC - British Library ...
In the aerodynamic shape design, the drag prediction has always been an extremely challenging missio...
Preliminary design or feasibility study is the first stage13; of an aircraft design during which the...
The prediction and decomposition of drag associated to Propulsive System Integration (PSI) is invest...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/143019/1/6.2017-0960.pd
Preliminary design or feasibility study is the first stage13; of an aircraft design during which the...
SIGLEAvailable from British Library Document Supply Centre- DSC:8670.19(RAE-TM-AERO--2146) / BLDSC -...
The drag prediction workshop series (DPW), held over the last six years, and sponsored by the AIAA A...
The goal of this thesis is to improve the wave drag estimation techniques in the aircraft conceptual...