![]() |
Quote:
As has been said before - the buffet region of flight has 'depth' due to washout and the progressive nature of the stall across the wingspan. It's possible for a pilot experienced on type to know how much he can pull through the buffet before a full-blown stall & consequent stall and/or flick will occur. The 'buzz' or 'nibble' does not necessarily presage an imminent stall, it just indicates that the inner part of the wing has exceeded max AoA, the airflow has separated from that surface and is impinging on the elevator. Quote:
W. |
Quote:
Regarding buffeting it is a highly unstable flight regime by def. Generally a localized buffeting zone is set artificially during the design phase to warn the pilot that is entering the stall flight regime. The buffeting is caused by a major recirculation of flow above the wing. Thus being unstable by definition. The Lift force ad pitching moment oscillating around a certain value cause the "shaking". Aeroelasticity plays also its role here needing more washout to give a safety margin (and more drag) (see http://www.aerospaceweb.org/question/planes/q0099.shtml) Winger , I can put my tail plane on top of a 10m pole above the fuselage and will still experience wing buffeting. ;) Regarding the F18 without going OT, if I wd hve been at Northrop I would hve design the buffeting point before the LERX vortex start to interact with the wings flow. A pilot would know then when he is entering high AoA flight regime. What I mean here is that the buffeting zone might be wider than in a conventional aircraft due to the interaction of conventional wing behavior and LERX. http://www.aerospaceweb.org/question/planes/q0176.shtml Regarding the Spitfire, the wider wing chord being rather flat (the max camber line being slightly frwd than conventional design), the pitchng moment is rather stable with AoA. This is good if you want to fit a variety of diverse equipment in a fighter aircraft but nasty when it comes to deal with a stall regime (IvanK that might give you some souvenir of teh Fr delta fighter spin ;) ) In particular once such aircraft is committed in a spin, it is more stable here than an other aircraft with shorter wing chord and more rounded airfoil (there I wld like readers fans of RoF to think abt the barn door wing profiles of British WWI planes). That said, it is mandatory to warm young pilots about the nasty behavior of such an aircraft in the spin. Then they will be more cautious in fight and the "turnability" of a Spitfire will vary greatly with the experience of its pilot. That's all we said here as I can understand with Crumpp writing and I think this shld be in the sim (I was saying very much the same thing years ago with IL2). Obviously an experienced fighter pilot will laugh of "the danger of being in a spin". But wait... Germans have shown the world twice that you don't win an air-war with experienced fighters pilots. That's all abt teh Legion Condor and the Hurricane, the experteen and the P51 or the WWI JastaCirkus and SPADs. Note : Writing this, I remember a Spit WWII WCO commenting the guncam footage of various pilots that were convinced they have hit their prey and demonstrating to them that they hve missed mostly because their plane were always drifting. This tells us a lot of how they were flying those planes that required much more attention than conventional aircraft when manoeuvring aggressively (of course not more than the early supersonics) PS: it's a great discussion we hve here :grin: |
Quote:
Hardly the description of the Spitfire's very hard and pronounced buffet as related by the NACA and its effects on turning performance confirmed in the Spitfire Mk I notes. |
I just thought I'd give some historical perspective on this.
I've got lots of BoB RAF pilot's accounts, a recurring theme from the top pilot's is "riding the buffet" Geoff Wellum mentions it in 'First Light' And I've seen it repeated quite often. Also, when the RAE were conducting the mock dogfights against a 109 they found that in every case where the 109 managed to get behind the Spitfire, it could stay there. when they looked at why, they found that the RAF pilot's were easing off when the buffeting started, when in fact they could have flown it on the edge and even tightened it slightly. It fits with contemporary accounts from both sides, with plenty of cases of each out-turning the other. As is usually the case, the more familiar the pilot is with his plane the better the chances of survival were. Some flew it on the edge, some flew it as per the handbook. |
Quote:
Quote:
If you have no other way to determine that point, it works for practical purposes. Gee, that is exactly what I have said!! Quote:
Quote:
Pilot......Aircraft Owner....several of them, they are great way to waste a lot of money! :) Oh yeah, aerobatics too... |
Quote:
What do you think the engineers are doing when they tell you those parameters?? Here is a secret....they are telling you how to get the maximum performance out of the aircraft, live to tell about it, and maybe be able to use the airplane on the next mission. |
Mh. I think the pilots were taught to fly their planes after the handbook.
With experience and in battle they started to feel the plane and forgot about the handbook resulting perhaps in situations where they were closer to the edge than written in the handbook. One should remember that air behaviour depends on much more than just velocity and angle of attack. It may well depend on current temperature, roughness of the skin of the plane, winds and gusts, air humidity ... |
Quote:
You can argue with Geoff Wellum all you want. You said that the pilot's notes say to ease off when buffeting occurrs. Geoff Wellum, for one, didn't do this, and they weren't too concerned with the rule book or the maths of it either, they did what they had to to survive. I've also read of plenty of WEP abuse, bent airframes, bale outs when lost ( i.e. not bothered about using the airplane again) I think the engineers were conservative in their pilot's notes. |
Quote:
Quote:
Let's look at what the reality of operating aircraft has to say about the Pilot Operating Instructions: Quote:
Quote:
If you read this primer on Pilot Operating Instructions, you will find that for most maximum performance there is ONLY one point or airspeed that maximum performance can be obtained. That point is linked to the physical design of the aircraft and is given to the pilot by the engineers. There is nothing to be "conservative" about. Additionally, the margins are such there is very little room engineering wise to be "conservative" and still produce a machine that flys. Read and enjoy!! http://www.faa.gov/library/manuals/a...apter%2010.pdf |
Quote:
Geoff Wellum - " In a Spitfire, just before the stall, the whole aircraft judders, it's a stall warning, if you like. With practice and experience you can hold the plane on this judder in a very tight turn. You never actually stall the aircraft and you don't need to struggle to regain control because you never lose it. A 109 can't stay with you." Time and time again people push machines past their operational limits, some live some die, that's not the point. The point is that 'riding the buffet' happened, for real. Geoff Wellum did it, as did many many other Battle of Britain pilots. As for the reality of flying aircraft, what's your experience of flying Spitfires in combat? I'll take my info from people who know what they are talking about, because they were there, thanks. Quote:
It's simply not the truth. I'll say it again, The RAE themselves (They conducted the 109 vs Spitfire mock dogfights) found that the reason in initial tests a Spitfire could not shake a 109 of it's tail was because the pilot's were backing off as soon as the buffet set in, when in fact it was possible to fly with the juddering and make a tighter turn. So max turning at least was achieved by not following 'the book' Quote:
Quote:
|
All times are GMT. The time now is 07:25 PM. |
Powered by vBulletin® Version 3.8.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright © 2007 Fulqrum Publishing. All rights reserved.