Titchener et al., 2013 - Google Patents
The effects of various vortex generator configurations on a normal shock wave/boundary layer interactionTitchener et al., 2013
- Document ID
- 11671241962043771582
- Author
- Titchener N
- Babinsky H
- Loth E
- Publication year
- Publication venue
- 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
External Links
Snippet
Within the inlet of high-speed air-breathing air-vehicles, it is often desirable to employ some form of flow control to increase inlet performance and flexibility. 1, 2 Traditionally, this has been achieved using a bleed system which removes a portion of the near-wall flow through …
- 230000035939 shock 0 title abstract description 22
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
- Y02T50/16—Drag reduction by influencing airflow
- Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
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