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Reinmar Horten describe las verdaderas condiciones del IAME en la decada del 50
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<blockquote data-quote="Brunner" data-source="post: 257656" data-attributes="member: 70"><p><strong>IA 37 , Ia 48</strong></p><p></p><p>Continuando con la tarea de refutar las leyandas urbanas y paparruchadas que han diseminado <em> "urbi et orbi</em>" ciertos pseudo-hiostoriadores incluyo las opiniones de Horten sobre las verdaderas posibilidades del IAME </p><p></p><p><strong>The I. Ae. 38 and 48 Delta Jets</strong></p><p></p><p><strong><em>Tests on two high speed delta wing projects, began with models that were catapulted into the sea at speeds up to 200 km/hr. By landing in water, they could usually be recovered intact. We used a pointed symmetrical airfoil, that had some interesting characteristics. </em></strong></p><p><strong><em>Wind tunnel tests revealed that an eddy would form on the top of the wing, behind, and about parallel to the leading edge. The diameter of the eddy grew with increasing angle of attack, and at the same time moved to the rear. It seemed appropriate to locate the elevons in the area of the eddies, to boost their effectiveness, and maintain their response even at 30-40 angle of attack. Then we discovered that the suction of the eddy was greet enough at low speeds, to cause a negative control surface pressure!</em></strong></p><p><strong><em></em></strong></p><p><strong><em>To further study these phenomena, a full size glider, with a prone pilot was built, complete with dummy engines. The test aircraft was towed aloft by a Ju 52, and later by a DC 3. About 150 hours of flight testing was performed with the I. Ae. 37.</em></strong></p><p><strong><em></em></strong></p><p><strong><em>The two place supersonic I. Ae. 48 was designed and ready to be built by the end of 1959, and metal parts for the production of two I. Ae. 37 s were delivered, when we were ordered to stop the work. The reason was given as "lack of funds". <strong> Perhaps our project was too advanced for a developing country"</strong></em></strong></p><p><strong></strong></p><p><strong><strong>Lo gracioso del caso:</strong></strong></p><p><strong>Que al menos dos "supuestos historiadores" en sus obras se han referido a un caza naval cataputable que desarrollo Horten...por cierto.eso es completamente falso,m ya que Horten indica que debido a la falta de materia prima, (hasta faltaba la madera balsa para los modelos a escala del IA 37) debieron lanzar a estos modelos con una catapulta sobre el Lago San Roque. Aqui laverdadera imagen del IA 37 cataputable, de la cual que estos falsificadores de la historia han pretendido convertir en un caza naval ala volante a reaccion,sin cola y catapultable <img src="/foros/styles/default/xenforo/smilies/biggrin.png" class="smilie" loading="lazy" alt=":D" title="Big Grin :D" data-shortname=":D" /> <img src="/foros/styles/default/xenforo/smilies/biggrin.png" class="smilie" loading="lazy" alt=":D" title="Big Grin :D" data-shortname=":D" /> <img src="/foros/styles/default/xenforo/smilies/biggrin.png" class="smilie" loading="lazy" alt=":D" title="Big Grin :D" data-shortname=":D" /> </strong></p><p><strong><img src="http://i2.photobucket.com/albums/y28/Brunner-yel/brunner-yel%20II/IA37delta_model_1.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" /></strong></p></blockquote><p></p>
[QUOTE="Brunner, post: 257656, member: 70"] [b]IA 37 , Ia 48[/b] Continuando con la tarea de refutar las leyandas urbanas y paparruchadas que han diseminado [i] "urbi et orbi[/i]" ciertos pseudo-hiostoriadores incluyo las opiniones de Horten sobre las verdaderas posibilidades del IAME [b]The I. Ae. 38 and 48 Delta Jets[/b] [B][I]Tests on two high speed delta wing projects, began with models that were catapulted into the sea at speeds up to 200 km/hr. By landing in water, they could usually be recovered intact. We used a pointed symmetrical airfoil, that had some interesting characteristics. Wind tunnel tests revealed that an eddy would form on the top of the wing, behind, and about parallel to the leading edge. The diameter of the eddy grew with increasing angle of attack, and at the same time moved to the rear. It seemed appropriate to locate the elevons in the area of the eddies, to boost their effectiveness, and maintain their response even at 30-40 angle of attack. Then we discovered that the suction of the eddy was greet enough at low speeds, to cause a negative control surface pressure! To further study these phenomena, a full size glider, with a prone pilot was built, complete with dummy engines. The test aircraft was towed aloft by a Ju 52, and later by a DC 3. About 150 hours of flight testing was performed with the I. Ae. 37. The two place supersonic I. Ae. 48 was designed and ready to be built by the end of 1959, and metal parts for the production of two I. Ae. 37 s were delivered, when we were ordered to stop the work. The reason was given as "lack of funds". [b] Perhaps our project was too advanced for a developing country"[/b][/I][b][/B] [B]Lo gracioso del caso:[/B] Que al menos dos "supuestos historiadores" en sus obras se han referido a un caza naval cataputable que desarrollo Horten...por cierto.eso es completamente falso,m ya que Horten indica que debido a la falta de materia prima, (hasta faltaba la madera balsa para los modelos a escala del IA 37) debieron lanzar a estos modelos con una catapulta sobre el Lago San Roque. Aqui laverdadera imagen del IA 37 cataputable, de la cual que estos falsificadores de la historia han pretendido convertir en un caza naval ala volante a reaccion,sin cola y catapultable :D :D :D [IMG]http://i2.photobucket.com/albums/y28/Brunner-yel/brunner-yel%20II/IA37delta_model_1.jpg[/IMG][/B] [/QUOTE]
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Guerra desarrollada entre Argentina y el Reino Unido en 1982
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Reinmar Horten describe las verdaderas condiciones del IAME en la decada del 50
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