From 2a56f714a54e38039d03c5bc0ffbae283f3fbff1 Mon Sep 17 00:00:00 2001 From: Marco Luigi Gaibotti <marco.gaibotti@skywarder.eu> Date: Wed, 19 Feb 2025 14:32:26 +0000 Subject: [PATCH] [documentation][Aerodynamics Optimisation] Fixed typos --- aerodynamicsOptimization/README.md | 4 ++-- 1 file changed, 2 insertions(+), 2 deletions(-) diff --git a/aerodynamicsOptimization/README.md b/aerodynamicsOptimization/README.md index 644dab35..6fbc0ce1 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 -- GitLab