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Thread: Lockheed Electra Model 10

  1. #76
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    yeah, it's cool looking, but, unfortunately,
    it's just pretty garbage. the only real value
    might be for another side view layout.

    with that in mind, i've continued
    the upper and lower lines of the aft nacelle
    on the side view drawing you sent.
    from there, i'll use that full nacelle profile
    to help build a new nacelle.
    then, we shall see how the wing intersects.
    i'll probably use 16 or 18 sided templates
    for the nacelle...26 is overkill.

    i've also delved into the wing profile templates.
    as stated numerous times,
    i am less than ecstatic with the three options.
    the flat bottom to the trailing edge
    on two of the options is ridiculously annoying.
    which leaves the simple seven sider.
    with all other template types,
    you can edit their layout
    after they have been constructed.
    not so with wing profile templates.
    line length and angles must be inserted
    correctly during construction.
    that's all well and good
    if you know the line lengths and angles.
    i don't...bitch, bitch, bitch...
    quit your whining, smilo, and get to work.

    side note;
    have you noticed,
    i love the word nacelle?

    have a great weekend.
    drink lots of fluids and stay cool
    sometimes the magic works.
    sometimes it doesn't.

  2. #77

    Bottom view!

    Hello Smilo,
    At last! I found a picture that includes a bottom view and I´ve e-mailed it to you. Here´s a screenshot too.
    the shape there is quite predictable, but at least it confirms what one could deduce from the side view.

    Using the 11-sided flat-bottom profile, perhaps once the wing and nacelle is completed, the trailing edge
    of the flat bottom panel can be untied and brought forward, and the edge of the top panel there could be
    lifted, and an extra panel inserted, which would correct the trailing edge of the wing.

    Then, the forward vertical leading edge panel could be untied, brought backwards, and
    split into two to give the leading edge a sharp front.
    Cheers,
    Aleatorylamp
    Attached Thumbnails Attached Thumbnails bottom view.jpg  
    "Why make it simple if you can also make it complicated?"

  3. #78
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    email received...in a word, FANTASTIC!
    incredible detail and clarity...thank you.

    and with interesting soviet markings.

    will most likely spend the weekend
    playing with wing profile template configurations
    and will then, seriously consider your idea.
    i'm also considering the use of two separate,
    but, overlapping wing profile template classes.
    it might be too complex..we shall see.

    i sure wish i knew how to hack this program
    and simply improve the template options.
    while i was in there, i'd also move the delete button
    or at least, make it ask if i want to delete a chain.
    i've accidentally hit that damned thing,
    one too many times.
    bottom line, i don't know how to hack the program,
    so, i'll have to be careful,
    make do with what i've got
    and save, save, save.
    i'm actually thinking of setting a timer
    to go off every ten minutes,
    just to remind me to hit the save button.
    sometimes the magic works.
    sometimes it doesn't.

  4. #79
    Hello Smilo,
    What is interesting in the bottom view I suppose is that the wheel well includes a narrower forward open section to cater for the landing gear strut. On other planes the strut had a plate that would cover that section, so only half the wheel would remain visible outside the well, and this plate would also act as an air-brake when the gear was extended. On the Electra it seems that it was simplified - although the gear did have mudguards!

    Regarding the wing profile and nacelle parts intersection, we´ll see how the results of the different possibilities develop, and then take a decision on the best solution to be used.
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  5. #80
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    progress (?) report;

    have i ever mentioned, i'm scattered?
    can't stay focused on a task?
    probably, borderline Attention Deficit Disorder.
    whatever...i deal with it.

    the point being, i decided to rework the wing.
    can't have a good intersection without it, right?
    spent quite a while getting the biconvex (7 side) template
    to fit inside your hand drawn profile.
    but, finally got it done...close enough.

    INTERUPTION!...

    i received the latest set of pictures and noticed
    the nacelle shot with wings removed,
    which in turn got me to thinking
    about cleaning up that exposed chord.

    OH, WAIT...
    didn't the other plans
    have bulkheads and a chord?
    yup...sure did.
    so, making a long story longer,
    i cropped out that chord,
    cleaned it up and now have
    a pretty good working example.
    that done, i set up an ad2k rough draft
    with the seven main vertices
    and have now connected the dots.
    what i have, is what looks like a biconvex(7) template.

    if i had a printer, i'd make a hard copy
    and use a protractor to measure the angles
    so i could easily transpose them
    to the ad2k profile template creator.
    but, no...i get to hunt and peck
    until i figure them out.

    hmmm, maybe it would be easier
    and save time, if i'd just copy the drawing
    to a flash drive and go get it copied in town.

    by the way, do you have the length
    of the chord if it was placed mid fuselage?
    sometimes the magic works.
    sometimes it doesn't.

  6. #81
    Hello Smilo,
    I see you are working very hard indeed, trying out different
    possibilities!

    The equivalent of the chord of the wing profile at the fuselage
    centerline would be 12.9 ft. The position of the leading edge
    would be at +4.2 ft, and the trailing edge at -8.7 ft. of CoG.

    Then, profile thickness at the nacelle centerline is 2 ft, but along
    the fuselage centreline, it would be 2.5 ft.

    Hope this helps! Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  7. #82
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    yes, it does, very much in deed, thank you.

    while i have your attention,
    at the risk of being critical,
    (which i am not)
    where did you come by your chord profile?
    was is from the side plan.jpg,
    highlighted in green?
    the reason i ask is that yours seems to be wider
    in proportion than the example DD
    in the upper left corner of Top-plan.JPG
    granted, the DD example is mid wing,
    but, the thickness discrepancy is substantial.

    update;
    i just ran the numbers for length to thickness ratio.
    the root wing profile, 12.155 long by 2.706 wide.
    dividing length by width, i get 4.492
    at fuselage center, 12.9/2.5= 5.16
    now the kicker. using the DD example,
    i could only count pixels and got 156/27= 5.778

    so, my question...which ratio do you want to use?
    or, do i have it all wrong?
    sometimes the magic works.
    sometimes it doesn't.

  8. #83
    Hello Smilo,
    Yes, I see what you mean.
    I had taken the measurements from the front and top view drawings. There seems to be a discrepancy with the dimensions on the side-view drawing which I hadn´t noticed before. I wasn´t using those because the red and light-green lines there were drawn in by hand by myself, and could perhaps be a bit off! I´m terribly sorry.
    In red, I´ve drawn in the sizes for the chord length and thickness on the top and front view drawing. Would you be OK with that? I´ll e-mail it to you too, because of the resolutioin.
    Cheers,
    Alńeatorylamp
    Attached Thumbnails Attached Thumbnails Top-plan-.jpg  
    "Why make it simple if you can also make it complicated?"

  9. #84
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    no need to be terribly sorry.
    things happen...don't worry about it.
    please email the modified drawings.

    have been up for a few hours tonight.
    am setting up a grid to layout
    the chord profile at 12.9 x 2.5.
    will then use it to build a biconvex template
    to fit inside a new hand drawn chord profile.

    ....starting to crap out, so, it's back to bed.

    i won't get much done tomorrow,
    will make the hour trip to the ferry terminal
    to pick up a family member flying into seattle.
    sometimes the magic works.
    sometimes it doesn't.

  10. #85
    Hello Smilo,
    I just noticed I had sent the e-mail with the top-view and front-view drawings as a reply to the SOH Forum notification...
    where it will be ignored! So, I´ve just sent it to you!
    It was easier to use those views because of the continuation in straight lines toward the fuselage centreline.
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  11. #86
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    to say the least,
    the past couple weeks have been a struggle.
    with the frustration of trying to figuring out
    the the ad2k wing profile template procedures
    being compounded by the big monitor
    slowly giving up the ghost,
    i finally had to step back for a bit.

    yesterday, i took a bite of the bullet,
    broke down and bought a new 48 inch tv/monitor.
    ...what a difference a few hundred dollars makes.
    now, i can actually, see what i'm doing.
    what a concept.
    the next step is to motivate the self
    to attack the profile template issue again....
    sometimes the magic works.
    sometimes it doesn't.

  12. #87
    Hello Smilo,
    We are having such a hot summer here that it´s hard to do anything on the computer.
    I was trying out a few work-arounds for this wing template thing, but none worked.
    Let´s see what I can do as soon as it gets a bit cooler.
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  13. #88
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    thought i had something, too,
    but, it didn't work, either.
    will keep trying.

    be safe
    sometimes the magic works.
    sometimes it doesn't.

  14. #89
    Hello Smilo,
    There´s greater difficulty than expected for twins in AD2k as regards nacelle/wing vertex adjustment, which didn´t apply to single-engined plane modelling.
    Let´s see if and how it can be worked out.
    The bog-down is such that the more limited yet more familiar AF99 is again bekonning from a distance, and I´m once more tempted to switch over.

    Cheers,
    Aleatorylamp.
    "Why make it simple if you can also make it complicated?"

  15. #90
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    it's clear that detailed chord profiles
    were not a high priority
    when ad2k was designed.
    so it goes.

    i don't know how long i've been trying
    to just build a simple 8 sided profile template
    with the vertices where i want them.
    i type in the angles and coefficients,
    OK out of the template editor input panel,
    then, go back into it to double check.
    oh goody...
    the program has readjusted them for me.
    ...followed by a long line of profanity
    trailing off into the darkness.
    i neither want or need the numbers
    adjusted for me...thank you very much.
    leave them the hell alone.

    after a while, i gave up
    and built a simple 6 sider
    and a 7 side, biconvex profile template
    that align (close enough) with key vertices
    on the hand drawn chord.

    after a break, i'll continue
    to dink around with the 8 sider.

    i sure most of the ad2k problems
    are self inflicted, ie, operator error.
    i'm just stubborn enough
    to take it as a challenge
    and will continue to fight on.
    sometimes the magic works.
    sometimes it doesn't.

  16. #91
    Hello Smilo,
    I went through that ordeal too! Changes in any of the profile templates NEVER come out as you need! Frustrating indeed...

    I´m sure it´s a programming bug, and not the user not doing something correctly! Plus, the fact that there are only 3 profile templates to chose from, makes the whole thing questionable too. They did notice... but didn´t publish a bug-fix. They only improved the profile templates for AD2K2 - incompatible for our needs though!

    So, with this rather big let-down, I am coming to the conclusion that AD2K is fine for single engined planes, or maybe twin engined jets, with their engines attached to the rear fuselage.

    I doubt that it will be worth while to continue torturing ourselves with this issue!


    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  17. #92
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    au contraire mon frčre,
    you give up too easily.
    i, on the other hand,
    am a glutton for punishment.
    where there is a will,
    there is a way.
    i will not be thwarted
    and will continue to muddle on.

    this is "fun"(?)

    actually, the fun part
    is coming up with a solution.
    sometimes the magic works.
    sometimes it doesn't.

  18. #93
    Hello Smilo,
    OK, ok...
    If it´s not one way, then it´s another.
    If the worst comes to the worst, we´ll fit the nacelle panels manually!
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  19. #94
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    that it is, my friend, that it is.
    i'm reminded of a story
    about an old lady's epitaph,

    SHE DIED OF ODTAA

    one damned thing after another


    how about this?
    why don't we attack
    this issue from two fronts?
    when you have time,
    build a wing, from fuselage center
    to pre-cap tip using af99.
    make the chord as complex as you want.
    if possible, add chord "bulkheads"
    at flap and aileron locations.
    bulkheads, both inside and outside
    of the nacelle would be a bonus.
    when done, send me the afx files
    to import into ad2k.
    remember, no structures or components.

    i'll continue trying to solve
    the profile template fiasco.
    the nice thing about templates,
    is that they can be covered,
    moved and resized to reflect
    the angle and taper of the wing.
    that's, basically, why i'm bothering with them.

    thinking about this,
    it's not a multi-engine issue.
    to my mind, it's more
    of a poor wing template options issue.
    i, obviously, am asking for much more
    than the program has to offer.
    i may be kidding myself, but,
    i feel that, if i can come up with
    a satisfactory basic profile template,
    i will be happy.
    actually, there's more to it than that,
    but, you get the idea...right?
    sometimes the magic works.
    sometimes it doesn't.

  20. #95
    Hello Smilo,
    Thanks!
    OK then: I´ll make an AF99 wing with an 11 or 12-sided profile, starting from the fuselage centreline.
    I´ll insert bulkheads at fuselage centre-line and wall, at nacelle-centre and inner and outer walls, and at wing-tip base - also at inner aileron end (outer end coincides with wing-tip base),
    Flaps were of the kind that came down under the wing, and seen from the top there´s no cut-out.

    I understand that the 11 or 12 wing-panels are to be in one piece each, going from the fuselage centre to the wing-tip base.
    Nose to the grindstone!
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  21. #96
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    eleven or twelve panel wing would be great.
    ...while i'm in wish mode,
    how about six chord bulkheads?
    one fuselage center
    one about a foot out from the fuselage wall
    one about a foot in from the inner nacelle wall
    one nacelle center
    one about a foot out from the nacelle wall
    and finally, one at the wing tip

    i sure hope that isn't too much to ask for
    sometimes the magic works.
    sometimes it doesn't.

  22. #97
    Hello Smilo,
    No, no problem! Will do.
    I´ll send it to you as soon as I get it done.
    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  23. #98
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    thank you, i look forward to it.
    as always, no rush.

    made some progress with the simple 8 last night.
    nothing to get excited about, just baby steps.
    but, i believe it was progress.
    sometimes the magic works.
    sometimes it doesn't.

  24. #99
    Hello Smilo,
    OK, so attached herewith are the AF99 wing parts for Lockheed L-10 Electra:
    6 Wing-profile bulkheads:

    -Central fuselage line bulkhead
    -1 ft out from fuselage wall
    -1 ft inside from nacelle
    -Central Nacelle
    -1 ft out from nacelle
    -Wing tip base

    15 Wing panels:
    -8 top panels, "w-panel1" to "w-panel7"
    -7 Wing under panels, "w-panel-u1" to "w-panel-u7"

    The wing-profile has 13 vertices. Have a look to see if everything´s ok!

    Cheers,
    Aleatorylamp
    "Why make it simple if you can also make it complicated?"

  25. #100
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    that was quick.
    thank you, Stephan.
    downloaded and will transfer
    to the design machine now.
    will report back, asap
    sometimes the magic works.
    sometimes it doesn't.

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