Author:
Colliss S. P.,Babinsky H.,Nübler K.,Lutz T.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Reference21 articles.
1. StanewskyE.DéleryJ.FulknerJ.GeisslerW. “Synopsis of the Project Euroshock,” Drag Reduction by Passive Shock Control: Results of the Project EUROSHOCK, Vol. 80, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag, Berlin, 2002, pp. 1–124.
2. StanewskyE.DéleryJ.FulknerJ.de MatteisP. “Synopsis of the project Euroshock II,” Drag Reduction by Shock and Boundary Layer Control: Results of the Project EUROSHOCK II, Vol. 56, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer-Verlag, Berlin, 1997, pp. 1–81.
3. Shock control on a swept wing
4. Shock-Wave/Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings
5. Numerical and Experimental Validation of Three-Dimensional Shock Control Bumps
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