Holden et al., 1995 - Google Patents
Measurements of boundary layer transition on cones at angle of attack for Mach numbers from 11 to 13Holden et al., 1995
- Document ID
- 13405127075692343317
- Author
- Holden M
- Bower D
- Chadwick K
- Publication year
- Publication venue
- Fluid Dynamics Conference
External Links
Snippet
The process of boundary layer transition is of key importance in hypersonic vehicle design and has been the focus of many investigations. Several key review papers discuss the complexity of the transition phenomena (see Morkovin'. 2? Reshotko3, and Mack4) Tne …
- 238000005259 measurement 0 title description 54
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