Fix PDF export from VSCode
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.ipynb_checkpoints/MD11-ECON-CRZ v3-checkpoint.ipynb
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9551
.ipynb_checkpoints/MD11-ECON-CRZ v3-checkpoint.ipynb
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@ -11,7 +11,7 @@ Second column is FF per engine in kg/hr
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Third column is IAS
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Third column is IAS
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- If single value, apply to all weights
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- If single value, apply to all weights
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- If multiple values, apply to respective weights (delimited with `,`)
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- If multiple values, apply to respective weights (delimited with `,`)
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-
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Fourth column is MACH
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Fourth column is MACH
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- If single value, apply to all weights
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- If single value, apply to all weights
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- If multiple values, apply to respective weights (delimited with `,`)
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- If multiple values, apply to respective weights (delimited with `,`)
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@ -28,7 +28,7 @@ First index is weight (equates to the lines in the file)
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Second index is CI (equates to the columns in a line)
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Second index is CI (equates to the columns in a line)
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- Must be in range $[0, 999]$
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- Must be in range $[0, 999]$
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# Format of raw curves
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# Format for raw curve tables
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2d matrix of curve parameters
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2d matrix of curve parameters
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Columns delimited with `;` \
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Columns delimited with `;` \
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@ -47,3 +47,15 @@ $$
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Extract parameters $a,b,c$ from the table \
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Extract parameters $a,b,c$ from the table \
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$x$ is the CI and must be in range $[0,999]$ \
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$x$ is the CI and must be in range $[0,999]$ \
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$f(x)$ is the mach number for the given altitude, weight, CI, and MMO
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$f(x)$ is the mach number for the given altitude, weight, CI, and MMO
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# Conversion of weight to index
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$$f(x) = \frac{x - 140}{10}$$
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$x$ is weight (see range restrictions where applicable)\
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$f(x)$ is the resulting index for the LUTs
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# Conversion of altitude to index
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$$f(x) = \frac{x - 250}{20}$$
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$x$ is altitude (see range restrictions where applicable)\
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$f(x)$ is the resulting index for the LUTs
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MD11-ECON-CRZ v3.html
10514
MD11-ECON-CRZ v3.html
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19103
MD11-ECON-CRZ v3.ipynb
19103
MD11-ECON-CRZ v3.ipynb
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