Abstract
Using a vorticity form of the Navier-Stokes equations the effects of nonlinearity on the development and receptivity of crossflow disturbances in the Swept Hiemenz boundary-layer are investigated. Steady perturbations are generated using wall suction and blowing that are distributed periodically as either a strip or point holes. The method, size and the location of the forcing are shown to significantly influence the receptivity of the crossflow within the boundary-layer. Perturbations excited by periodic blowing holes have considerably larger amplitudes than those generated by suction holes or strips. A linear log relationship is derived that relates the receptivity amplitude of the linear only disturbances with the chord position that the nonlinear primary Fourier perturbation attains a state of equilibrium: location that the maximum absolute amplitude of the primary disturbance shows distinct differences to the linear only solution. Further the size of the chordwise velocity perturbation at the location corresponding to equilibrium can be predicted directly from the linear only solutions. Thus, if the receptivity amplitude of the linear perturbation is smaller than some given threshold magnitude, nonlinear flow characteristics can be predicted directly from the computationally less expensive linear analysis.
Original language | English |
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Title of host publication | 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 |
Subtitle of host publication | St. Petersburg; Russian Federation; 7 September 2014 through 12 September 2014 |
Editors | Alexander Filatyev |
Place of Publication | Stockholm Sweden |
Publisher | International Council of the Aeronautical Sciences |
Number of pages | 8 |
ISBN (Electronic) | 3932182804 |
ISBN (Print) | 9781634394116 |
Publication status | Published - 1 Jan 2014 |
Externally published | Yes |
Event | Congress of the International Council of Aeronautical Sciences 2014 - St. Petersburg, Russian Federation Duration: 7 Sept 2014 → 12 Sept 2014 Conference number: 29th |
Conference
Conference | Congress of the International Council of Aeronautical Sciences 2014 |
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Abbreviated title | ICAS 2014 |
Country/Territory | Russian Federation |
City | St. Petersburg |
Period | 7/09/14 → 12/09/14 |
Other | ICAS was established in 1957 as a non-government, non-profit scientific organization with the mission to advance knowledge and facilitate collaboration in aeronautics. Today ICAS brings together 32 states from five continents. Among ICAS members are major world aerospace companies. |
Keywords
- Boundary-layer
- Crossflow
- Disturbance development
- Nonlinearity
- Receptivity