That trolley accumulator looks pretty swish, good work Blu_2.
Aaaahhh!!!!! That’s a relief, it’ll help bolster the meds.
I am desolated, depression has set in, my Post Meteor Update Syndrome (PMUS) is in overdrive. The tablets aren’t working – I am, let’s face it, a mess. Must have update, must have update, must have ……………. gaaaaahhhhhhhh!!!!!!!
How on earth was he able to keep his cloth cap on??
Earliest example of a flush riveted hat retainer. 😀
That’s right stand and glare at it – that’ll get some cooperation 😡
Well who’s been a busy boy then – like the trick with the tire. Keep up the good work.
Good to see no problems with the upper rudder. Thanks for the update Blu_2.
Thanks for the update – that rudder area is rapidly turning into a can of worms isn’t it. But keep up the good work.
Hmmm …. probably was overall aerodynamically best suited to a conventional tail.
I’m not sure if you can call theM-tail on the Bonanza a “modification” since it was originally designed and flown with it.
There is an interesting section on the tail selection in Those Incomparable Bonanzas by Larry Ball. He notes the feature was first tested as an experiment for application on future high speed aircraft on a AT-10 trainer in 1943.
It doesn’t say whether it was purely a Beech initiative or if it was done at the behest of NACA (now NASA) or a university.Specifically it states:
-On low wing types, it gets the horizontal stabilizer out of the turbulence caused by the wing at some speeds.
-It reduced surface to fuselage intersections which cut drag.
-The AT-10 testbed didn’t offer any weight savings but the designers felt that if it were designed into a h del from the beginning, a weight savings could be realized.
-Based on some flight test data from the AT-10, it was believed that a V-tail offered better soon recovery. Apparently, in conventional tail designs, the horizontal stabilizer, when stalled, can blank out part of the vertical stabilizer and rudder. It was felt the o figure AT-10 had better soon recovery than the stock model.At any rate, the Bonanza underwent extensive (and probably unprecedented) wind tunnel studies for a “light” aircraft.
In other words, it wasn’t designed and built by some blokes in a shed. The primary designer was Ralph Harmon and the team that designed the very successful and long lived (32 years) Twin Beech Model 18.
Was there any difference in the aerodynamic features of the rest of the Bonanza i.e. wings, fuselage and engine thrust line etc. between the V tailed version and the conventionally tailed version. Perhaps there isn’t and the removal of the V tail actually worked to actually enhance performance by removing an unrecognised problems Certainly the Me 109 and the Polish aircraft are really just a conventionally tailed aircraft that have had the empennage changed to a V. It really appears to me that those aircraft that have worked successfully with a V tail in whatever form have close attention paid to the fuselage and its aerodynamic function as a part of the lift rather than simply as a streamlined protective enclosure for the crew and payload. But I could be wrong.
Now while I really am not an expert or even particularly knowledgeable on the subject of aerodynamics I suspect that where the V tail has been successfully applied it is part of a design package that includes integrating the design of the whole airframe including fuselage and wings so that the V tail itself is an effective component of the overall aerodynamic package. The Fouga Magister and the F117 exhibit that integration of features. However in the case of the Bonanza, the Polish design and the earlier mentioned Me 109 experiment the V tail appears to be a modification restricted only to the rear fuselage and even then more as tinkering with a design than seeking a fully integrated design.
Thanks Blu_2.
Not unlike the effects on ground and air crew of the XF-84 Thunderscreech which had a propeller revolving with supersonic tip speeds. Nausea, headaches etc.
Thanks for the update.
Thanks for the update Blu_2. It’s a pity about the upper mount casting.