TWITT ArchiveAdditional Materials  | 
          
| Akaflieg Karlsruhe AK-X | 
            
              
               The AK-X flying wing
                sailplane is being built by the students of Akaflieg
                Karlsruhe in Germany. The AK-X is promising to be the
                next big thing in high performance Standard Class (15 m)
                sailplanes. The AK-X is in fact a continuation of the
                legendary SB-13, exploiting the invaluable experience
                gained by its predecessor. The Akaflieg Karlsruhe
                expects a performance in par with larger tailed
                sailplanes (18 m??) without the (admittedly few)
                shortcomings of the SB-13. Let's hope that they succeed.
                The Akaflieg posts a Youtube video reporting the
                progress of the project almost every month. Here is the
                link: https://www.youtube.com/c/AkademischeFliegergruppeamKITKarlsruhe/videos 
              And also find below the
                site of the Akaflieg Karlsruhe, where more interesting
                material regarding the AK-X can be found ( this material
                is in German, but a translator will do the job): AK-X | Akaflieg Karlsruhe 
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| Horten
                - Stability Considerations in Sweptback Wings  | 
            
              
               R. Horten's "Stability
                Considerations in Sweptback Wings," in which he presents
                his theory of making the highly tapered sweptback flying
                wing platform (which is the configuration that he used
                for his flying wings throughout his life) tip-stall
                proof and spin proof (the "C-Point" theory). Strangely,
                this is a paper I hadn't read before (I discovered it a
                couple of months ago). All of those fellows who have
                studied K. Nickel's book "Tailless Aircraft in Theory
                and Practice" will be familiar with the theory of R.
                Horten presented in the attached paper, because in fact
                K. Nickel was closely cooperating with him. K. Nickel
                himself also in his book "Tailless Aircraft in Theory
                and Practice" gives credits Horten when explaining the
                theory behind the "C-Point" and its significance in
                flying wings. The even more fascinating thing, is that
                we still use his theory even today,
                especially us RC aeromodellers, when locating the
                correct CoG of a new flying wing: the well known
                graphical chord construction in fact finds the Mean
                Geometric Chord, the 25% of which is the "C- Point" or
                "Geometric Neutral Point "!!! (See this link for how to
                do it: Flying wing CG calculator.) 
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| Ho II Test Flight | https://www.youtube.com/watch?v=GjXr5w3M4mc Includes detailed notes by Reimar Horten.  | 
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| Ho XVc Pappenheim | 
            Nikolas provided this video of a
              demonstration flight of the Ho XVc Pappenheim. | 
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| Ashkenas - Tailless Aircraft Performance Improvements with Relaxed Static Stability  | 
            This I. L. Ashkenas paper "Tailless
              Aircraft Performance Improvements with Relaxed Static
              Stability." This paper is fascinating because in fact it
              is a continuation of Northrop's work on flying wings,
              solves the problems arising with the stability configured
              flying wing, and clearly gives hints on how the B-2 bomber
              operates. | 
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| Klingberg Wing Mk
              II  | 
            Rol Klingberg is now trying to finish and fly his second flying wing rigid hang glider, the "Klingberg Wing MKII." He occasionally presents his progress through YouTube videos on his channel (https://www.youtube.com/c/KlingbergWingMkII/videos). | |
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