From 64d9710a127c6ec595b52259a757987edd3e5e4d Mon Sep 17 00:00:00 2001
From: andy <andy>
Date: Tue, 29 Mar 2005 19:05:47 +0000
Subject: [PATCH] Add a section for camber.

---
 Docs/README.yasim | 3 +++
 1 file changed, 3 insertions(+)

diff --git a/Docs/README.yasim b/Docs/README.yasim
index 1c2c8cc66..5b549de55 100644
--- a/Docs/README.yasim
+++ b/Docs/README.yasim
@@ -88,6 +88,9 @@ wing:     This defines the main wing of the aircraft.  You can have
                      constrained well by the solution process, and may
                      require tuning to get throttle settings correct in
                      high AoA (approach) situations.
+          camber:    The lift produced by the wing at zero angle of
+                     attack, expressed as a fraction of the maximum
+                     lift produced at the stall AoA.
 
 hstab:    These defines the horizontal stabilizer of the aircraft.
           Internally, it is just awing objects and therefore work the