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Verified Commit 799726cf authored by Thomas Lambert's avatar Thomas Lambert :helicopter:
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docs(readme): fix typos

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...@@ -186,7 +186,7 @@ same order. These arguments can be of two types: ...@@ -186,7 +186,7 @@ same order. These arguments can be of two types:
Some functions then extend these inputs by using various optional arguments. Some functions then extend these inputs by using various optional arguments.
### extendpolar #### extendpolar
This function extends known $`C_l`$ and $`C_d`$ polars to the full range of This function extends known $`C_l`$ and $`C_d`$ polars to the full range of
angle of attacks [-180; 180]. This is especially useful when studying rotors and angle of attacks [-180; 180]. This is especially useful when studying rotors and
...@@ -207,10 +207,10 @@ import af_tools.extendpolar ...@@ -207,10 +207,10 @@ import af_tools.extendpolar
| 'method' | `'Viterna'` | `'Viterna'` | | 'method' | `'Viterna'` | `'Viterna'` |
| 'limit' | `'stall','limit'` | `'last'` | | 'limit' | `'stall','limit'` | `'last'` |
### plotpolars #### plotpolars
Plots the following polars: $`C_l-\alpha`  ,   $`C_d-\alpha`$ Plots the following polars: $`C_l-\alpha`$  ,   $`C_d-\alpha`$
 ,   $`C_m-\alpha`$  ,   $`C_l/C_d-\alpha`  ,   $`C_m-\alpha`$  ,   $`C_l/C_d-\alpha`$
 ,   $`C_l-C_d`$.  ,   $`C_l-C_d`$.
```matlab ```matlab
...@@ -220,7 +220,7 @@ plotpolars(Polar) ...@@ -220,7 +220,7 @@ plotpolars(Polar)
plotpolars(alpha, cl, cd, cm) plotpolars(alpha, cl, cd, cm)
``` ```
### findstall #### findstall
Finds the stall angle of attack and the associated $`C_l`$ and $`C_d`$. Finds the stall angle of attack and the associated $`C_l`$ and $`C_d`$.
...@@ -231,7 +231,7 @@ import af_tools.findstall ...@@ -231,7 +231,7 @@ import af_tools.findstall
[alpha_s, cl_s, cd_s] = findstall(alpha, cl, cd) [alpha_s, cl_s, cd_s] = findstall(alpha, cl, cd)
``` ```
### findzerolift #### findzerolift
Finds the zero-lift angle of attack and the associated $`C_d`$. Finds the zero-lift angle of attack and the associated $`C_d`$.
...@@ -242,7 +242,7 @@ import af_tools.findzerolift ...@@ -242,7 +242,7 @@ import af_tools.findzerolift
[alpha_zeroL, cd_zeroL] = findzerolift(alpha, cl, cd) [alpha_zeroL, cd_zeroL] = findzerolift(alpha, cl, cd)
``` ```
### findcllinearrange #### findcllinearrange
Finds the range of angles of attack for which the $`C_l`$ can be considered Finds the range of angles of attack for which the $`C_l`$ can be considered
linear. linear.
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