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Aggregate A9 (A4b)
- Quorneng
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First a recap on progress so far.
This is the ultimate aim. An RC 'winged' V-2 (A4b) as an EDF and in Depron.
EDF right at the back with a very short duct to give maximum static thrust.
It should be light enough to hand launch and belly land.
The issue is the EDF will have to obtain all its air from cheat holes and these will be positioned on the rear of the fuselage so will in effect be somewhat shielded from the direct airflow. Ultimately it would be nice to have these covered with spring loaded doors.
Before embarking on the full build I intend to make just the rear section with the EDF and cheat holes to determine the best method of construction and the effect the cheat holes have on the static thrust.
Something like this:
First the inner cone, planked in 2mm Depron.
At this point it became obvious that to keep each inlet smooth and of the right cross sectional area would require them to have quite a complex shape. Whilst I could visualise the require shape I could not see a way of actually making them in planked Depron.
Unfortunately the most likely solution would not use the inner cone shape that I had already made!
Rather than start again I decided to continue and finish the test duct but with a simple inlet duct shape that would be relatively easy to make however they would be less that ideal aerodynamically.
Although a bit disappointed at my construction failure I can take some comfort that the EDF and its inlet is the biggest unknown part of this build so 'development' at this stage should improve the chances of it actually flying reasonably well.
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you do pick some difficult subjects Simon.
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- Quorneng
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First 4 supports.
These represent the outside profile and provide location for the EDF.
The first of the exterior planks.
More skin planking around the intake opening. The planks continue right to the end of the fan body.
A view down one of the four identical intakes.
The intakes are bigger than strictly necessary and their internal shape is not ideal but building this has certainly given me some ideas on where to improve their shape and more important how to build them!
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you do like unusual subjects.
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- Quorneng
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However I fear I have 'blown' my only 50 A ESC - when I connected the battery there was a really load crack, I thought at the time is sounded more than the usual capacitor charging. 2 seconds later I noticed the wires were getting warm in my hands! Unplugged the battery pronto.
The reason was obvious. In my temporary electrical 'lash up' just to test the fan was rotating the right way I had a positive to negative connection! :woohoo: . ESC don't like being connected the wrong way. Doh!
I only had a spare 20A ESC but even so it blows a lot of air on just 15A!
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- Quorneng
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A bit bigger than first thought at 20" span and 48" long. The fuselage is close to 6" diameter at its maximum.
It will likely be built in 3 sections with the nose and middle as half shells over the plan. The tail section will probably be built as a single unit. It will be built first as it is the most complex shape and carries all the mechanical bits!
Still only a guestimate at this stage but with a high C 1800mAh 3s it should come out a bit below 20oz all up.
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A quick question, have you thought about how you're going to launch it. With a 6" dia fus, it may be a bit difficult to get your fingers to grip.
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lovely idea simon, hope it all works ok
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- Quorneng
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Launching is an issue. This is the method I use on my V-1 which by chance is also 6" diameter.
The shallow reinforced finger hole is just behind the COG, the sand paper finger grips are a bit in front so it is held like this.
Note I launch left handed although it would work just a well in the other hand.
Publish? May be!
Before I start work on the 'flight' version of the tail end I have been looking at the possibility of spring loaded doors.
The current arrangement of the test duct means the inlets are significantly over size. As it 'submerges' into the fuselage each has an area of just over 1700 mm sq 'normal' to the airflow. At close to 7000 mm sq for the four gives a total area that is over twice the FSA. :huh:
This suggest there is some room to alter the shape of the inlet duct to allow a long single door to both fit the fuselage aperture and hinge down to give a reasonably smooth path to the duct with an area of 1/4 the FSA.
I will modify one of the inlets on the test duct to experiment.
I have drawn the over hung elevons to the scale size (although I am a bit dubious of the accuracy of some of the 3 views) but they look very large and delicate for something that could achieve close to 2000 mph! :woohoo: Perhaps I should not complain as such generous proportions will be a distinct advantage at 30mph!
I have found this period photo.
It would seem to confirm each elevon was indeed something like the drawing.
Models of the A4b were tested in the supersonic wind tunnel at Peenemunde.
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- Quorneng
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A slight change in plan as this bit will now be built in one piece - vertically - as I did with the V-1.
The 9 formers.
All but the smallest are internally flanged rings to give the best strength to weight ratio.
There will be a lot on empty space inside!
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- one tenor
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- johnpcalex@gmail.com
www.astronautix.com/lvs/a4b.htm There is more on the net if you Google or whatever ..
Anything will fly given enough power
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- Quorneng
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Much easier as it has a constant taper so each plank is simply a straight edged triangle.
The full nose section represents just over 1/3 of the total fuselage length.
I think the wings next. One piece skin tip to tip?
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- Quorneng
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It weighs 24g (0.83 oz)
When the glue is fully hard It will need a bit of filling and gentle sanding.
As far as I have been able to find out the wings were of a typical 'supersonic' section, sharp leading edge, fully symmetrical, maximum thickness near to 50% and pretty thin so that is what mine will have!
A one piece 2mm Depron skins top and bottom.
As a full 'stressed skin' structure it has no spars just Depron spacers and only 3 ribs!
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- THE BLACKBIRD
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Fantastic
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