Relevant bibliographies by topics / Onera M6

Contents

  1. Journal articles
  2. Book chapters
  3. Conference papers

Academic literature on the topic 'Onera M6'

Author: Grafiati
Published: 20 February 2023

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Onera M6.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Onera M6"

1

Алексеенко, С. В. "ЧИСЛЕННОЕ МОДЕЛИРОВАНИЕ ОБТЕКАНИЯ КРЫЛА ONERA M6." Bulletin of Dnipro University. Series: Mechanics 26, no. 5 (April 26, 2018): 57. http://dx.doi.org/10.15421/371806.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Mayeur, J., A. Dumont, D. Destarac, and V. Gleize. "Reynolds-Averaged Navier–Stokes Simulations on NACA0012 and ONERA-M6 Wing with the ONERA elsA Solver." AIAA Journal 54, no. 9 (September 2016): 2671–87. http://dx.doi.org/10.2514/1.j054512.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Balan, Aravind, Michael A. Park, William K. Anderson, Dmitry S. Kamenetskiy, Joshua A. Krakos, Todd Michal, and Frédéric Alauzet. "Verification of Anisotropic Mesh Adaptation for Turbulent Simulations over ONERA M6 Wing." AIAA Journal 58, no. 4 (April 2020): 1550–65. http://dx.doi.org/10.2514/1.j059158.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

NAMBU, Taisuke, Atsushi HASHIMOTO, Takashi AOYAMA, and Tetsuya SATO. "Numerical Analysis of the ONERA-M6 Wing with Wind Tunnel Wall Interference." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 58, no. 1 (2015): 7–14. http://dx.doi.org/10.2322/tjsass.58.7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Batina, John T. "Accuracy of an unstructured-grid upwind-Euler algorithm for the ONERA M6 wing." Journal of Aircraft 28, no. 6 (June 1991): 397–402. http://dx.doi.org/10.2514/3.46040.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Goodheart, Kevin A., and Gunter H. Schnerr. "Condensation on ONERA M6 and F-16 Wings in Atmospheric Flight: Numerical Modeling." Journal of Aircraft 42, no. 2 (March 2005): 402–12. http://dx.doi.org/10.2514/1.5137.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Nejati, A., and K. Mazaheri. "Application of the adjoint optimisation of shock control bump for ONERA-M6 wing." European Journal of Computational Mechanics 26, no. 5-6 (October 12, 2017): 557–83. http://dx.doi.org/10.1080/17797179.2017.1386022.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Johan, Zdeněk, Kapil K. Mathur, S. Lennart Johnsson, and Thomas J. R. Hughes. "A case study in parallel computation: Viscous flow around an ONERA M6 wing." International Journal for Numerical Methods in Fluids 21, no. 10 (November 30, 1995): 877–84. http://dx.doi.org/10.1002/fld.1650211008.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Li, Zong Zhe, Zheng Hua Wang, Lu Yao, and Wei Cao. "A Combined Global Coarsening Method for 3D Multigrid Applications." Applied Mechanics and Materials 236-237 (November 2012): 1049–53. http://dx.doi.org/10.4028/www.scientific.net/amm.236-237.1049.

Full text
Abstract:
An automatic agglomeration methodology to generate coarse grids for 3D flow solutions on anisotropic unstructured grids has been introduced in this paper. The algorithm combines isotropic octree based coarsening and anisotropic directional agglomeration to yield a desired coarsening ratio and high quality of coarse grids, which developed for cell-centered multigrid applications. This coarsening strategy developed is presented on an unstructured grid over 3D ONERA M6 wing. It is shown that the present method provides suitable coarsening ratio and well defined aspect ratio cells at all coarse grid levels.
APA, Harvard, Vancouver, ISO, and other styles
10

Hejranfar, Kazem, and Ramin Kamali Moghadam. "A Comparative Study of Two Preconditioners for Solving 3D Inviscid Low Speed Flows." Applied Mechanics and Materials 110-116 (October 2011): 423–30. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.423.

Full text
Abstract:
In the present study, two preconditioners proposed by Eriksson, and Choi and Merkel are implemented on a 3D upwind Euler flow solver on unstructured meshes. The mathematical formulations of these preconditioning schemes for the set of primitive variables are drawn and their eigenvalues and eigenvectors are compared with each others. A cell-centered finite volume Roe's method is used for discretization of the 3D preconditioned Euler equations. The accuracy and performance of these preconditioning schemes are examined by computing low Mach number flows over the ONERA M6 wing for different conditions.
APA, Harvard, Vancouver, ISO, and other styles
More sources

Book chapters on the topic "Onera M6"

1

Takakura, Yoko, Satoru Ogawa, and Tomiko Ishiguro. "Inviscid and viscous flow simulations around the ONERA-M6 wing by TVD schemes." In 11th International Conference on Numerical Methods in Fluid Dynamics, 553–57. Berlin, Heidelberg: Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/3-540-51048-6_91.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Achard, Timothée, Christophe Blondeau, and Roger Ohayon. "High-Fidelity Aero-Structure Gradient Computation Techniques. Application to the Onera M6 Wing." In Advances in Structural and Multidisciplinary Optimization, 483–99. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-67988-4_37.

Full text
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Onera M6"

1

Michal, Todd R., Frederic Alauzet, Adrien Loseille, Loïc Frazza, David L. Marcum, and Dmitry S. Kamenetskiy. "Comparing Anisotropic Error Estimates for the Onera M6 Wing RANS Simulations." In 2018 AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0920.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Ricardo G. da Silva, João Luiz F. Azevedo, and Edson Basso. "Numerical Simulation of ONERA M6 Wing using the BRU3D CFD Code." In 23rd ABCM International Congress of Mechanical Engineering. Rio de Janeiro, Brazil: ABCM Brazilian Society of Mechanical Sciences and Engineering, 2015. http://dx.doi.org/10.20906/cps/cob-2015-0197.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Silva, Ricardo G., Joao Luiz F. Azevedo, and Edson Basso. "Simulation of ONERA M6 Wing Flows for Assessment of Turbulence Modeling Capabilities." In 54th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-0549.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Hart, Pierce, and Sven Schmitz. "Application of Partial-Pressure Field Drag Decomposition to the ONERA M6 Wing." In AIAA AVIATION 2021 FORUM. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-2555.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Thomas, Bryce Z., and Ramesh K. Agarwal. "Application of Wray Agarwal Turbulence Model for Predicting Transonic Flow over ONERA-M6 Wing." In AIAA SCITECH 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-0463.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Kaya, Mustafa, Munir Elfarra, and Ferhat Kadioglu. "Investigation of the Effect of Taper Stacking Location on Drag Force for ONERA M6 Wing." In AIAA Scitech 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-2123.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Gleize, Vincent, Antoine Dumont, Julien Mayeur, and Daniel Destarac. "RANS simulations on TMR test cases and M6 wing with the Onera elsA flow solver (Invited)." In 53rd AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1745.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Nilsson, Stefan, Hua-Dong Yao, Anders Karlsson, and Sebastian Arvidson. "Effects of Viscosity and Density on the Aeroelasticity of the ONERA M6 Wing from Subsonic to Supersonic Speeds." In AIAA AVIATION 2022 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-3670.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Mohamed, Kaveh, Kurt Sermeus, and Eric Laurendeau. "A Fast Grid Deformation Algorithm for Aerodynamic Shape Optimization." In ASME 2010 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/detc2010-28782.

Full text
Abstract:
A mesh movement algorithm suitable for aerodynamic design optimization problems is presented. It involves B-spline surface construction, projection and evaluation on B-spline faces for the surface mesh movement, as well as inverse-distance and 2D/3D TFI interpolations for the volume mesh deformation. The algorithm is fast and exhibits an excellent parallel efficiency. It is used to deform the surface and volume mesh of an ONERA-M6 wing undergoing several planform changes. The quality of the deformed mesh is preserved as long as the difference between the initial surface mesh and the B-spline surface model is small. A good agreement reported between the flow simulation results on the deformed mesh and those obtained on initial fixed mesh.
APA, Harvard, Vancouver, ISO, and other styles
10

Jasak, Hrvoje, and Gregor Cvijetić. "Implementation and Validation of the Harmonic Balance Method for Temporally Periodic Non–Linear Flows." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-56254.

Full text
Abstract:
An efficient method for tackling non-linear, temporally–periodic incompressible flows is presented in this paper. Assuming temporally fully periodic flow, Harmonic Balance method deploys Fourier transformation in order to formulate transient problem as a multiple quasi-steady state problems. The method is implemented in OpenFOAM and developed for a general transport equation and incompressible Navier–Stokes equations. Validation is presented on three test cases: oscillating scalar case for scalar transport validation, a flow around a 2D NACA airfoil and a 3D Onera M6 wing for turbulent incompressible Navier–Stokes validation. For all test cases Harmonic Balance results are compared to transient simulation results. Verification of the model is performed by changing the number of harmonics for all test cases.
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the extended bibliographies on the topic 'Onera M6' for particular source types:
Journal articles
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography