From 26cf8ccc244bfb7f4837ebf3a81c8606f1f576e1 Mon Sep 17 00:00:00 2001
From: Ruben Di Battista <ruben.dibattista@skywarder.eu>
Date: Fri, 7 Oct 2016 17:42:53 +0200
Subject: [PATCH] Update README.md

---
 README.md | 2 +-
 1 file changed, 1 insertion(+), 1 deletion(-)

diff --git a/README.md b/README.md
index 66edc66..b734a85 100644
--- a/README.md
+++ b/README.md
@@ -15,7 +15,7 @@ The filename is optional. Without it the parser will look for the `for006.dat' f
 
 ## Output File ###
 The Output file is composed by two structures: `Coeffs` and `State`. 
-`Coeffs` contains all the aerodynamic coefficients interpolated over the 4 states (AoA, Mach, Altitude, Sidesplip angles) and the struct `State` contains the set of states (Aoa, Mach, Altitude, Sideslip Angle) the coefficients have been calculated on and the position of the center of gravity.
+`Coeffs` contains all the aerodynamic coefficients interpolated over the 4 states (AoA, Mach, Altitude, Sideslip angles) and the struct `State` contains the set of states (Aoa, Mach, Altitude, Sideslip Angle) the coefficients have been calculated on and the position of the center of gravity.
 
 ```
 Coeffs = 
-- 
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