Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.2 9/18/84; site pecnos.UUCP Path: utzoo!watmath!clyde!cbosgd!ihnp4!houxm!vax135!petsd!pecnos!don From: don@pecnos.UUCP (Don Hopkins) Newsgroups: net.aviation Subject: Re: Conditions for stall Message-ID: <121@pecnos.UUCP> Date: Wed, 2-Oct-85 13:58:01 EDT Article-I.D.: pecnos.121 Posted: Wed Oct 2 13:58:01 1985 Date-Received: Thu, 3-Oct-85 06:16:33 EDT References: <763@infopro.UUCP> <2900005@hpcvrd.UUCP> <2717@hplabsc.UUCP> <737@terak.UUCP> Organization: Perkin-Elmer SSD, Tinton Falls, N.J. Lines: 21 > ... What is this nonsense the FAA (and others) say about being able to > stall a plane in any attitude at any airspeed? Try to stall a plane > at Vne. It won't stall. (You'd have to pull maybe 15 G's, and the > plane will come apart instead :-) > -- > Doug Pardee -- CalComp -- {calcom1,savax,seismo,decvax,ihnp4}!terak!doug This may be true for the type of airplane you fly, but consider the modern jet fighter that is capable of withstanding high-G forces without coming apart. In a high speed dive if the pull-up is too abrupt it is certainly possible to stall the aircraft despite the fact you may be doing mach 1 or greater. Name........: Donald F. Hopkins Company.....: Perkin-Elmer Data Systems Group US Mail.....: 106 Apple St., Tinton Falls, N.J. 07724 Phone.......: 201-758-7268 UUCP..(work): ...!{decvax,ucbvax,ihnp4}!vax135!petsd!pecnos!don (home): ...!{decvax,ucbvax,ihnp4}!vax135!petsd!pecnos!buslog!dfh Brought to you by Super Global Mega Corp .com