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Hmm.......
The outlines of the wing...sorry...fuselage..(or should it be 'hull'..? ), form a fully symmetrical "wing section" (although very thick), with a totally neutral stab shown on plan, i.e. no decalage at all, thus requiring a slightly raised nose when flying level. As this nose-up attitude makes the "thing" fly, we cannot do anything about it, though by raising the stab T/E a little, thus providing an initial decalage of couple of degree or so, wouldn't trimming be easier...?...and the airflow over the stab getting more "clean" as well....?..."flying wing-wise".... ![]() Thinking loud, again....
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Power-wise, the original design flew with a sport type 1/2A engine, such as a Baby Bee 049. If memory serves, those put out about 1/20 of a horsepower on mild fuel and a 6 x 3 prop, or around 37 watts. Allowing for motor inefficiency, I'll need about 50 watts of input power to get that. And my high altitude location (5300 feet above seal level) might be another factor. So many variables... |
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Joined Mar 2009
198 Posts
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The lifting body concept was a logical development in which engineers tried to design a reentry vehicle which maximized volumetric efficiency and yet had sufficient gliding capability to land like an airplane rather than landing by parachute. A round ball has the greatest ratio of volume to surface area, and the Russians did indeed use the round ball shape at first. Not only does the round ball have optimum volumetric efficiency, but it also is most immune to localized heating during re-entry. Sharp edges, corners, fins & wings get hot much faster than a blunt, rounded shape. The Americans quickly went to the shape of a missile nose cone. The nose cone isn't quite as efficient from a volume standpoint, but it takes advantage of the existing shape of the missile nose. But it was necessary to turn the nose cone around backwards for reentry. Both the sphere and the nose cone have a glide ratio of essentially zero. So the lifting body is the minimum modification to a nose cone which would have an adequate lift to drag ratio so it could be landed without a parachute. The first lifting body flown by NASA was really nothing more than one half of a missile nose cone shape. Theoretically, you could have put two lifting bodies back to back on top of the booster and they would become the nose cone. The invention of thermal protection materials (such as tiles) was a game changer. Now we could put wings on a re-entry vehicle and not have them burn off. So the Space Shuttle was made possible by the advent of high temperature insulation. Prior to having high temperature insulation it would have been necessary to cover a vehicle with an ablator, which burns away on re-entry and unfortunately changes the shape of the vehicle and gives it a very rough surface. By the way, virtually all of the key lifting body engineers were or had been modelers. And some of the first "proof of concept" lifting bodies were stick and tissue paper free flight models. Sorry for being so long winded, Dick |
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Joined Mar 2009
198 Posts
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For anyone who would like to see a video of the very first lifting body model airplane, take a look at the youtube below. The video has some factual errors, leading one to believe that the first model was radio controlled and was dropped from a larger RC model. But that "first" model was strictly free flight and was towed aloft by a conventional powered model which did have rudder and tow release control. Remember, this as 1962 and radios were not simple, not small, and certainly not cheap. Short clips can be seen at about 1:45 to 2:00 and is B&W 8mm film. The red and yellow "mother ship" seen there is a later development, from about 1967. By then we had a little more budget and proportional radios (wow ! Into the big time).
The fellow speaking, Dale Reed, built that first model (and the towplane) at home on his own time and with his own money. His wife took the 8mm movie at a local dirt strip airport. Dick
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That is indeed interesting and it's surprising to find that this lifting body project was the brain child of a single engineer. Must have been quite a ride, with a sink rate of 3600 feet per minute.
Not sure about a hatch yet, but I've had good luck with magnetically held hatches in the past. |
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