===================================================================
RCS file: /home/cvs/OpenXM_contrib/gnuplot/demo/Attic/airfoil.dem,v
retrieving revision 1.1.1.2
retrieving revision 1.1.1.3
diff -u -p -r1.1.1.2 -r1.1.1.3
--- OpenXM_contrib/gnuplot/demo/Attic/airfoil.dem	2000/01/22 14:16:04	1.1.1.2
+++ OpenXM_contrib/gnuplot/demo/Attic/airfoil.dem	2003/09/15 07:09:29	1.1.1.3
@@ -1,5 +1,5 @@
 #
-# $Id: airfoil.dem,v 1.1.1.2 2000/01/22 14:16:04 maekawa Exp $
+# $Id: airfoil.dem,v 1.1.1.3 2003/09/15 07:09:29 ohara Exp $
 #
 # This demo shows how to use bezier splines to define NACA four
 # series airfoils and complex variables to define Joukowski
@@ -121,7 +121,7 @@ airfoil_y2(t, thick) = mean_y(z_x(t)) - z_y(t, thick)
 airfoil_y(t) = mean_y(z_x(t))
 airfoil_x(t) = mean_x(z_x(t))
 set nogrid
-set nozero
+set nozeroaxis
 set parametric
 set xrange [-0.1:1.1]
 set yrange [-0.1:.7]