Delay of Transition Using Forced Damping

By: Nasa, National Aeronautics and Space Adm

Several experiments which have reported a delay of transition are analyzed in terms of the frequencies of the induced disturbances generated by different flow control elements. Two of the experiments employed passive stabilizers in the boundary layer, one leading-edge bluntness, and one employed an active spark discharge in the boundary layer. It is found that the frequencies generated by the various elements lie in the damping region of the associated stability curve. It is concluded that the creation of strong disturbances in the damping region stabilizes the boundary-layer and delays the transition from laminar to turbulent flow. Exton, Reginald J. Langley Research Center NASA/TM-2014-218551, L-20496, NF1676L-20143

• Format: Paperback
• Language: English
• ISBN: 1793986142
• ISBN13: 9781793986146
• Release Date: January 1
• Publisher: Independently Published
• Length: 34 Pages
• Weight: 0.23 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"