From 11b583b54ead74820a5bc8e5f2a2c0af14f74f96 Mon Sep 17 00:00:00 2001
From: aross <aross>
Date: Sat, 30 Nov 2002 03:24:27 +0000
Subject: [PATCH] Document the new "idrag" attribute on wing objects.

---
 Aircraft-yasim/README.yasim | 7 +++++++
 1 file changed, 7 insertions(+)

diff --git a/Aircraft-yasim/README.yasim b/Aircraft-yasim/README.yasim
index b2ba7968e..392a1b812 100644
--- a/Aircraft-yasim/README.yasim
+++ b/Aircraft-yasim/README.yasim
@@ -65,6 +65,13 @@ wing:     This defines the main wing of the aircraft.  You can have
                     Defaults to zero.
           dihedral: The dihedral angle of the wing.  Positive angles
                     are upward dihedral.  Defaults to zero.
+          idrag:    Multiplier for the "induced drag" generated by this
+                    surface.  In general, low aspect wings will
+                    generate less induced drag per-AoA than high
+                    aspect (glider) wings.  This value isn't
+                    constrained well by the solution process, and may
+                    require tuning to get throttle settings correct in
+                    high AoA (approach) situations.
 
 hstab:    These defines the horizontal stabilizer of the aircraft.
           Internally, it is just awing objects and therefore work the