Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.1 (Tek) 9/26/83; site tekred.UUCP Path: utzoo!watmath!clyde!burl!ulysses!mhuxr!mhuxn!mhuxm!mhuxi!mhuxh!mhuxv!mhuxt!houxm!vax135!cornell!uw-beaver!tektronix!tekred!normb From: normb@tekred.UUCP (Norm Babcock ) Newsgroups: net.aviation Subject: ROC Message-ID: <325@tekred.UUCP> Date: Wed, 17-Apr-85 20:34:54 EST Article-I.D.: tekred.325 Posted: Wed Apr 17 20:34:54 1985 Date-Received: Fri, 19-Apr-85 00:21:25 EST Organization: Tektronix, Redmond OR Lines: 21 After reviewing the C-152 handbook, the significance of the heading of the table I get rate-of-climb, fuel, distance, etc., from for various altitudes, hit me. The heading is for MAXIMUM rate of climb. Even though I make a stab at calculating this and that, correcting for temp, the actual performance is always less. I figured out then,(or remembered), that I don't like the deck angle at max climb, and always lower the nose for better visibility and cooling. My question is: is there a correction factor which works for different climb speeds? Is climb performance linear with speed? ROC would decrease, fuel would increase, time to TOC would increase, as would distance to TOC. Or does one have to play test pilot and make new tables? I realize a lot of pilots gas and go; and I do also, but sometimes I like to do a precision nav flight just for kicks. I would like to get a little better at forecasting a/c performance. Any ideas? tektronix!tekred!normb