diff --git a/aerodynamicsOptimization/README.md b/aerodynamicsOptimization/README.md
index 644dab356dd1540a46f4d832b204976bbf2054b5..6fbc0ce17549ad99b42cc7efefba42260e113d09 100644
--- a/aerodynamicsOptimization/README.md
+++ b/aerodynamicsOptimization/README.md
@@ -11,7 +11,7 @@ The following table shows the available optimisation parameters
 | Fins height      |    3   |                         -                         |
 | Fins sweep       |    4   |    Measured as distance between start of chords   |
 | Ogive length     |    5   |                         -                         |
-| Ogive shape      |  6, 7  | Valid for modified Haack: edits coefficinets p, C |
+| Ogive shape      |  6, 7  | Valid for modified Haack: edits coefficients p, C |
 | Boat-tail length |   8    |                         -                         |
 | Nosecone type    |    9   |                         -                         |
 
@@ -42,4 +42,4 @@ You can optimize the rocket and the boat tail or just the rocket, keeping the bo
 
 
 ## Output
-The output data consists in a set of optimization variables which allow the rocket to reach the maximum apogee with the chosen tolerance.
\ No newline at end of file
+The output data consists in a print of optimization variables which allow the rocket to reach the maximum apogee with the chosen tolerance.
\ No newline at end of file