X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FUIUCModel%2Fuiuc_iced_nonlin.cpp;h=30ac008fa5637fb57fc9a96fe5579e1548abf82d;hb=70b4f38ebccbafea664ed2310eaf990bd2b9edd8;hp=700092ae096a4ad79e1b9983b7a74fefc3254933;hpb=7289eaa8baafac56a3e32dedd5b77d3534d61c4a;p=flightgear.git

diff --git a/src/FDM/UIUCModel/uiuc_iced_nonlin.cpp b/src/FDM/UIUCModel/uiuc_iced_nonlin.cpp
index 700092ae0..30ac008fa 100644
--- a/src/FDM/UIUCModel/uiuc_iced_nonlin.cpp
+++ b/src/FDM/UIUCModel/uiuc_iced_nonlin.cpp
@@ -1,6 +1,6 @@
-//     SIS Twin Otter Iced aircraft Nonlinear model
-//     Version 020409
-//     read readme_020212.doc for information
+//     SIS Twin Otter Iced aircraft Nonlinear model
+//     Version 020409
+//     read readme_020212.doc for information
 
 // 11-21-2002 (RD) Added e code from Kishwar to fix negative lift problem at
 //            high etas
@@ -33,7 +33,7 @@ void Calc_Iced_Forces()
 	
 	
 	
-	alpha = Alpha*RAD_TO_DEG;
+	alpha = Std_Alpha*RAD_TO_DEG;
 	de = elevator*RAD_TO_DEG;
 	// lift fits
 	if (alpha < 16)