The P-51B Conversion

by Steve Griffiths - Summer 2001

 

This project was a joint design by Steve and Mike Briggs, based on Paul Janssens' original design. 

Our 40” span P-51D Mustangs built from a modified version of Paul Janssens’ plan had proved to be excellent fliers, managing not just to stay aloft in the light lift at the Lleyn Peninsula last August, but also to indulge in aerobatic manoeuvres, and generally behave to our satisfaction. The mods we made to the plan were primarily to substitute a built-up fuselage for the balsa-clad foam one, and to change the mainplane incidence, with appropriate adjustment of the tailplane to maintain a sensible decalage. Then, more recently, we were asked to build another as a birthday present for a friend who had recently lost his, but to produce it as a P-51 B/C version for which he had a preference.

Fortunately there is oodles of information available on Mustangs, so it didn’t take long to find some drawings and loft out a set (well, three, if you can call that a set) of rear upper-fuselage half-formers. A new model was built with the razor-back sides sheeted with 3/32” balsa, in place of the foam turtle-deck we had used on the D version. At the same time we incorporated a subsidiary half-longeron to reinforce the fuselage sides across the wing bay, where ours were showing some creasing alongside the main bulkhead; no doubt the effects of some less-than-perfect landings (i.e. most of them). A balsa block was carved as a canopy form, and in a short session with the electric fire and electric drill, a canopy was produced. When fitted it wasn’t just right, as it didn’t merge into the rear fuselage smoothly enough. Sandpaper and elbow-grease on the form easily remedied that, and a couple of acceptable canopies were soon made.

North American P-51 B Mustang by Steve Griffiths

Assembled, with a veneered white foam wing (but excluding all servo mounts, cockpit fittings and pilot), the whole model weighed under 12 oz. ready to cover, and was completed in spare time over a couple of weeks. It is expected to fly at an AUW of 20-21 oz, giving a wing loading of around 11.5 oz/sq.ft.

 

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