Copyright © Philip M. Parker, INSEAD. Terms of Use.
| Domain | Definition |
Aerospace | (Symbol CF). A measure of the amplification of thrust due to gas expansion in a particular nozzle as compared with the thrust that would be exerted if the chamber pressure acted only over the throat area. Also called thrust coefficient. (references) |
Source: compiled by the editor from various references; see credits. | |
Crosswords: NOZZLE THRUST COEFFICIENT |
| Specialty definitions using "NOZZLE THRUST COEFFICIENT": thrust coefficient. (references) |
Hexadecimal (or equivalents, 770AD-1900s) (references)4E 4F 5A 5A 4C 45 54 48 52 55 53 54 43 4F 45 46 46 49 43 49 45 4E 54 |
| Leonardo da Vinci (1452-1519; backwards) (references)
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Binary Code (1918-1938, probably earlier) (references)01001110 01001111 01011010 01011010 01001100 01000101 00100000 01010100 01001000 01010010 01010101 01010011 01010100 00100000 01000011 01001111 01000101 01000110 01000110 01001001 01000011 01001001 01000101 01001110 01010100 |
HTML Code (1990) (references)N O Z Z L E   T H R U S T   C O E F F I C I E N T |
ISO 10646 (1991-1993) (references)004E 004F 005A 005A 004C 0045 0054 0048 0052 0055 0053 0054 0043 004F 0045 0046 0046 0049 0043 0049 0045 004E 0054 |
Encryption (beginner's substitution cypher): (references)484960604639254425255535423749394040433743394854 |
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Copyright © Philip M. Parker, INSEAD. Terms of Use.
