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- From: mtc@hpcc01.corp.hp.com (Mark Cousins)
- Date: Thu, 19 Nov 1992 17:23:11 GMT
- Subject: Re: Exceed Vne or max G's first? (was Re: looping a non-acro aircraft)
- Message-ID: <87330003@hpcc01.corp.hp.com>
- Organization: HP General Systems Division
- Path: sparky!uunet!zaphod.mps.ohio-state.edu!sdd.hp.com!hpscit.sc.hp.com!scd.hp.com!hpscdm!hplextra!hpcc05!hpcc01!mtc
- Newsgroups: rec.aviation.misc
- References: <1992Nov5.121947.1266@eplrx7.es.duPont.com>
- Lines: 21
-
- In rec.aviation.misc, jfarrell@cloudbase (Jerry Farrell) writes:
-
- >Apparently so. I quote from the Flight Manual (POH) for the Schleicher
- >ASK-21:
-
- (nonpertinent material deleted)
-
- > True airspeed (TAS) is, however relevant for safety against flutter.
- > Therefore, one must take into account that with increasing altitude
- > the true airspeed is higher than the reading of the airspeed indicator
- > because of the increasing air density.
- ^^^^^^^^^^
-
- Shouldn't this read "decreasing"?
-
- Mark
- --
- Mark Cousins Hewlett-Packard Co. mtc@hpsemc.cup.hp.com
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