CFD simulations of infinite-swept wings with shock control bumps; parametric study Matlab files (.mat) contain a set of reduced data, obtained from batch post-processing of raw simulation files. Further information on contents and how to access file contents are contained in readme text files within data folders.EPSRC DT
© 2015, American Institute of Aeronautics and Astronautics Inc. All rights reserved. Results from wi...
Data Reduction technique for Wind tunnel testing of Aeroelastic models with case studies discussed
Datase to support article "Data-driven sparse reconstruction of flow over a stalled aerofoil us...
Supporting material: Franciolini, M. et al (2017). Efficient infinite–swept wing solver for s...
<p>Data accompanying the Experiments in Fluids paper entitled: Extremum seeking to control the ampli...
Shock control bumps offer the potential to reduce wave drag on transonic aircraft wings. However, mo...
Numerical and experimental studies have been performed to show the potential for drag reductions of ...
A method allowing a detailed investigation of the flow physics of shock control bumps (SCBs) on an u...
The data attached consists of .dat and .plt files which can be used to reproduce the figures found i...
Previous studies of transonic shock control bumps have often been either numerical or experimental. ...
Dataset for: Degregori, E. and Kim, J.W. Mitigation of transonic shock buffet on a supercritical ae...
Dataset in support of the article Data-driven determination of low-frequency dipole noise mechanisms...
Corresponding Flow article DOI: 10.1017/flo.2022.11 published in the Flow journal. This is the da...
This is the dataset that contains the data that are presented in the figures in the following paper:...
This deposit contains simulation configurations as well as analysis notebooks used in "The Sensitivi...
© 2015, American Institute of Aeronautics and Astronautics Inc. All rights reserved. Results from wi...
Data Reduction technique for Wind tunnel testing of Aeroelastic models with case studies discussed
Datase to support article "Data-driven sparse reconstruction of flow over a stalled aerofoil us...
Supporting material: Franciolini, M. et al (2017). Efficient infinite–swept wing solver for s...
<p>Data accompanying the Experiments in Fluids paper entitled: Extremum seeking to control the ampli...
Shock control bumps offer the potential to reduce wave drag on transonic aircraft wings. However, mo...
Numerical and experimental studies have been performed to show the potential for drag reductions of ...
A method allowing a detailed investigation of the flow physics of shock control bumps (SCBs) on an u...
The data attached consists of .dat and .plt files which can be used to reproduce the figures found i...
Previous studies of transonic shock control bumps have often been either numerical or experimental. ...
Dataset for: Degregori, E. and Kim, J.W. Mitigation of transonic shock buffet on a supercritical ae...
Dataset in support of the article Data-driven determination of low-frequency dipole noise mechanisms...
Corresponding Flow article DOI: 10.1017/flo.2022.11 published in the Flow journal. This is the da...
This is the dataset that contains the data that are presented in the figures in the following paper:...
This deposit contains simulation configurations as well as analysis notebooks used in "The Sensitivi...
© 2015, American Institute of Aeronautics and Astronautics Inc. All rights reserved. Results from wi...
Data Reduction technique for Wind tunnel testing of Aeroelastic models with case studies discussed
Datase to support article "Data-driven sparse reconstruction of flow over a stalled aerofoil us...
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