TeamGrumman-List Digest Archive

Thu 11/24/11


Total Messages Posted: 5



Today's Message Index:
----------------------
 
     1. 11:33 AM - Re: Fw: Flying with a level (Gary L Vogt)
     2. 12:27 PM - Re: Fw: Flying with a level (Doug Doty)
     3. 07:53 PM - Re: Re: Fw: Flying with a level (Bob Hodo)
     4. 08:43 PM - Re: Fw: Flying with a level (Doug Doty)
     5. 10:14 PM - Re: Re: Fw: Flying with a level (Gary L Vogt)
 
 
 


Message 1


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    Time: 11:33:23 AM PST US
    Subject: Re: Fwd: Flying with a level
    From: Gary L Vogt <teamgrumman@AOL.COM>
    I have nothing to hide. Besides, I think there are a lot of folks who would l ike the education even if they have nothing to add. Who knows, there may be a lurker out there with some valuable information. Gary Sent from my iPad On Nov 23, 2011, at 11:03 PM, Bob Hodo <bob.hodo@yahoo.com> wrote: > >>Did this go out to the list? I didn't see it. > > No, my last several emails have gone only to you, and Bob Steward, and Ned . I think Ned and Bob are kind of keeping it between the four of us as well , at least for now. > > Bob Hodo > > >


    Message 2


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    Time: 12:27:52 PM PST US
    Subject: Re: Fwd: Flying with a level
    From: "Doug Doty" <39marinette@gmail.com>
    You are right about Lurkers. I drag raced for 25 years and crave speed and efficiency, so don't think I am not enjoying the exchange of information, I am dying to pick up a little and smoke a certain mooney !!!!! -------- 1977 AA5B N28454, Fuel Totalizer, Lopresti Nose, Red Rudder Cap, 4 cyl. egt, stock otherwise. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=359129#359129


    Message 3


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    Time: 07:53:48 PM PST US
    From: Bob Hodo <bob.hodo@yahoo.com>
    Subject: Re: Fwd: Flying with a level
    It wasn't that I was trying to keep anything from the lurkers, as much as I was trying to organize my thinking, knew I was probably making some mental mis-calculations, etc. I had sent a 13 item list to Bob S, Ned, and Gary of a combo of facts and a ssumptions, and immediately got two corrections from Ned, and later a strin g from Gary. I won't re-print the errant first draft, but will come back later on with s ome ideas, or at least observations I have never seen addressed either here or on the grumman gang. I have not seen a word about any of this on the GG so far. It began with Ned asking a very reasonable question about whether a certain amount of split elevator might not be a lower drag arrangement. Then Ned said something about flying with a level on his canopy rails, so I had to go fly the cheetah and see what my level would show me. Now I have downloaded an inclinometer for both my droid x and my Motorola X oom, and am surprised at my first few readings. I have also been staring at a wing rib borrowed from Bob Steward.- I am c onvinced that we do not need to go into the experimental category to find s ome speed and economy that Roy Lo-Presti said was in there. .................... For the moment I will offer this:- Our canopy rails and the floor under t he front seat, and the HS appear to all be parallel to each other. When the flat bottom of the fuselage bends upwards, it does so at a 7 degre e angle.- I am told that is a significant number. When my cheetah is strait and level at 140 knots, the canopy rails are more than 1 degree ( 1.27 is my first measurement ) nose down.- That means th at rear section is 8.27 degrees nose down. I just don't see how that is not a problem from a fuselage drag standpoint, nevermind what the empenage is experiencing. Another thing most of you do not know is that our wings are NOT flat on the bottom.- They are flat with a 4+ degree bend just like the bottom of the fuselage has its 7 degree bend. The aft flat section of the wing sits two degrees nose down to the canopy r ails, the flat front section being just more than 2 degrees nose up.- By the time we reflex our flaps or ailerons or both, the bottom side of our wi ng is just horrible compared to that beautiful camber on the top. And then I walk across the maintenance hanger and look at that wing on the Cirrus SR22... Bob Hodo GADsden, AL,- I need to start smoking a pipe.


    Message 4


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    Time: 08:43:30 PM PST US
    Subject: Re: Fwd: Flying with a level
    From: "Doug Doty" <39marinette@gmail.com>
    I am always looking for some place to go so maybe I'll swing over that way and compare notes some day, I am going to Florida to get warm soon and Louisiana to visit a son healing from an Afghanistan wound a while back. I look at it. Doug... -------- 1977 AA5B N28454, Fuel Totalizer, Lopresti Nose, Red Rudder Cap, 4 cyl. egt, stock otherwise. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=359147#359147


    Message 5


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    Time: 10:14:49 PM PST US
    From: Gary L Vogt <teamgrumman@yahoo.com>
    Subject: Re: Fwd: Flying with a level
    This is the basic 64-415 airfoil. It really is a nice airfoil. Too bad the l eading edge was messed with: http://worldofkrauss.com/foils/1674 7 or 8 degree rise in the aft fuselage in flight, though not all that optimu m, is not that bad from a flow separation stand point. Just look at the aft e nd of an Aerostar. Crawl under your plane after filling it with 8 qts of oil and flying for an hour. The oil streaks are quite uniform. A while back, I p ut dye on the sides where the fuselage breaks. Not great but not all that ba d. Any chance of getting the ribs to build a 64-415 wing for a Tiger? Just an observation: look at the leading edge of a late AG5B. It's a lot s harper than a 70s era wing. Gary Sent from my iPad On Nov 24, 2011, at 7:51 PM, Bob Hodo <bob.hodo@yahoo.com> wrote: > It wasn't that I was trying to keep anything from the lurkers, as much as I was trying to organize my thinking, knew I was probably making some mental m is-calculations, etc. > > I had sent a 13 item list to Bob S, Ned, and Gary of a combo of facts and a ssumptions, and immediately got two corrections from Ned, and later a string from Gary. > > I won't re-print the errant first draft, but will come back later on with s ome ideas, or at least observations I have never seen addressed either here o r on the grumman gang. > > I have not seen a word about any of this on the GG so far. > > It began with Ned asking a very reasonable question about whether a certai n amount of split elevator might not be a lower drag arrangement. > > Then Ned said something about flying with a level on his canopy rails, so I had to go fly the cheetah and see what my level would show me. > > Now I have downloaded an inclinometer for both my droid x and my Motorola X oom, and am surprised at my first few readings. > > I have also been staring at a wing rib borrowed from Bob Steward. I am co nvinced that we do not need to go into the experimental category to find som e speed and economy that Roy Lo-Presti said was in there. > > .................... > > For the moment I will offer this: Our canopy rails and the floor under th e front seat, and the HS appear to all be parallel to each other. > > When the flat bottom of the fuselage bends upwards, it does so at a 7 degr ee angle. I am told that is a significant number. > > When my cheetah is strait and level at 140 knots, the canopy rails are mor e than 1 degree ( 1.27 is my first measurement ) nose down. That means that rear section is 8.27 degrees nose down. > > I just don't see how that is not a problem from a fuselage drag standpoint , nevermind what the empenage is experiencing. > > Another thing most of you do not know is that our wings are NOT flat on th e bottom. They are flat with a 4+ degree bend just like the bottom of the f uselage has its 7 degree bend. > > The aft flat section of the wing sits two degrees nose down to the canopy r ails, the flat front section being just more than 2 degrees nose up. By the time we reflex our flaps or ailerons or both, the bottom side of our wing i s just horrible compared to that beautiful camber on the top. > > And then I walk across the maintenance hanger and look at that wing on the Cirrus SR22... > > Bob Hodo > GADsden, AL, I need to start smoking a pipe. > > > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= ========================== ========= >




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