I hope to find some real numbers from others that have done this same conversion. I am about to start putting the wings to airframe and establishing geometry. The Javelin plans seem to indicate 24" longer airframe with the same horizontal reference line, the same Pacer tailfeathers, and the same Pacer 6.5 degrees down and 1.0 degree up horizontal stabilizer travel.
D&E plans for the wing, without knowing what airframe it's going on, show the front spar attach bolt centerline as 1.063" down from top of spar cap, and for the rear spar, 1.567" down from top of spar cap. These will establish the angle of incidence for the wing ie. the angle between the horizontal reference line of the fuselage and the CHORD LINE of the wing.
This configuration is what is proposed and before I move forward I am really hoping to hear what others have used and what their results were. I will use PA-18 tailfeathers, and a IO-375 powerplant with Catto 86x40 prop.
What I want to end up with is:
Ability to trim the tail down for landing in most forward loaded configuration ie. minimum fuel, pilot only. In order to get the angle of attack required to fly as slow as possible.
So for now I would really like to hear how others have done this wing, tail, and stretch geometry and how it worked out.
If there is a better location to post this request, please advise. Thanks to all who can help.
Scott
Edit: The Javelin stretch doesn't say where the tailpost is vertically in relation to horizontal reference line. They just give add-on tube lengths and specify to keep tailpost plumb. Where does it end up??
D&E plans for the wing, without knowing what airframe it's going on, show the front spar attach bolt centerline as 1.063" down from top of spar cap, and for the rear spar, 1.567" down from top of spar cap. These will establish the angle of incidence for the wing ie. the angle between the horizontal reference line of the fuselage and the CHORD LINE of the wing.
This configuration is what is proposed and before I move forward I am really hoping to hear what others have used and what their results were. I will use PA-18 tailfeathers, and a IO-375 powerplant with Catto 86x40 prop.
What I want to end up with is:
Ability to trim the tail down for landing in most forward loaded configuration ie. minimum fuel, pilot only. In order to get the angle of attack required to fly as slow as possible.
So for now I would really like to hear how others have done this wing, tail, and stretch geometry and how it worked out.
If there is a better location to post this request, please advise. Thanks to all who can help.
Scott
Edit: The Javelin stretch doesn't say where the tailpost is vertically in relation to horizontal reference line. They just give add-on tube lengths and specify to keep tailpost plumb. Where does it end up??
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