Copyright © Philip M. Parker, INSEAD. Terms of Use.
| Domain | Definition |
Aerospace | In fluid flow, layer next to a fixed boundary. The fluid velocity is zero at the boundary but the molecular viscous stress is large because the velocity gradient normal to the wall is large. See turbulent boundary layer.The equations describing the flow in the laminar boundary layer are the Navier-Stokes equations containing only the inertia and molecular viscous terms. (references) |
Source: compiled by the editor from various references; see credits. | |
Crosswords: LAMINAR BOUNDARY LAYER |
| Specialty definitions using "LAMINAR BOUNDARY LAYER": turbulent boundary layer. (references) |
Hexadecimal (or equivalents, 770AD-1900s) (references)4C 41 4D 49 4E 41 52 42 4F 55 4E 44 41 52 59 4C 41 59 45 52 |
| Leonardo da Vinci (1452-1519; backwards) (references)
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Binary Code (1918-1938, probably earlier) (references)01001100 01000001 01001101 01001001 01001110 01000001 01010010 00100000 01000010 01001111 01010101 01001110 01000100 01000001 01010010 01011001 00100000 01001100 01000001 01011001 01000101 01010010 |
HTML Code (1990) (references)L A M I N A R   B O U N D A R Y   L A Y E R |
ISO 10646 (1991-1993) (references)004C 0041 004D 0049 004E 0041 0052 0042 004F 0055 004E 0044 0041 0052 0059 004C 0041 0059 0045 0052 |
Encryption (beginner's substitution cypher): (references)463547434835522364955483835525924635593952 |
| 1. Crosswords 2. Orthography 3. Bibliography |
Copyright © Philip M. Parker, INSEAD. Terms of Use.
