Akaflieg Dresden D-B08 Wolfgang Pomnitz
Autre nom (ou nom en langue originelle) : Dresden Baunummer 8| DONNÉES GÉNÉRALES |
| Année du premier vol (ou de design, si seul projet) |
1929 |
| Pays | Allemagne |
| Designer(s) | SCHICHT, Friedrich |
| Premier constructeur | Akad. Fliegergruppe T. H. Dresden |
| Type d'appareil | Planeur |
| Fonction | Performance |
| SPÉCIFICATIONS TECHNIQUES |
| Envergure | 20 m |
| Longueur | -- |
| Hauteur | -- |
| Allongement | -- |
| Surface alaire | 18 m2 |
| Profil aile | Göppingen 527 |
| Masse à vide | 227.4 kg |
| Masse maxi | 297.4 kg |
| Charge alaire | 15.6 kg/m2 |
| Vitesse mini | -- |
| Vitesse maxi | -- |
| Finesse maxi | |
| Taux de chute mini | -- |
| Nb sièges | 1 |
| Structure | Bois et toile |
[Das Segelflug - collection J-M. Mesot]
[Pas de plan 3 vues connu]AUTRES INFORMATIONS
| Constructeur(s) |
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| Infos techniques | The "Dresden Academic Flying Group" likewise took part in the Rhön meeting 1929 with two aircraft. The unsupported high-wing monoplane "Baunmumer 8" possesses a strongly tapered trapeziform wing, in three sections and of two-spar construction. As far back as the rear spar the wing is surfaced with plywood so as to produce good torsional stiffness. This form of construction is similar to that of the "Elida," with the result that, what with an aspect-ratio of 1 to 21, its specific wing weight of 7.3 kg. per sq. metre was greater than that of any other machine at the meeting. The body possesses a rectangular cross-section with a large vertical edge at the end, so that the side elevation of the end of the body possesses a very considerable keel action. The horizontal stabilising fin is unsupported and is placed upon the upper surface of the body. The elevator itself is astonishingly small. Owing to the copious employment of plywood surfacing, the machine proved exceptionally heavy, and as owing to the heavy outer wing portions the moment of inertia about the longtitudinal and vertical axes must have been very considerable. There were at first some scruples on the part of the Technical Commission against allowing it unconditional admission. Various flights at the end of the meeting, as well as during very gusty weather, showed the aircraft to possess sufficient controllability. As a result of the high wingloading and the distortion of the long unsupported wing the machine flew astonishingly smoothly. | ||||||
| Histoire résumée | -- | ||||||
| Liens personnalités | SCHICHT, Fr. (Allemagne) |
SOURCES DOCUMENTAIRES
| Liens WEB | Site : UIUC Applied Aerodynamics Group's . Göttingen 527 airfoil. (2009-11-22) Site : UIUC Applied Aerodynamics Group's . Göttingen 527 fichier DAT. (2009-11-22) |
| Livres | Das Segelflugzeug par LANGSDORFF, Werner von (1931) [p. 56, 74, 79, 93, 135. Texte + 1 photo + specs]. Forschen-Bauen-Fliegen par LEMKE, Frank-Dieter & JACOB, Rolf (2010) [p. 20, 21. Texte + 1 photo + specs]. |
| Autres sources | Technical report of the Rhön glider meeting 1929, par A. Lippisch, Wasserkuppe, Rhön, The British Gliding Association Journal vol. 1 n° 3, janvier 1931 p 66-82. Publié in "Zeitschrift fiir Flugtechnik und Motorluftschriffahrt," volume 21, No. 4, p. 92 ; editeur R. Oldenbourg, Munich. Texte + specs. |
MODÈLES RÉDUITS
| Pas de plan ou kit référencé. |
Fiche n° 93 [Dernière mise à jour : 2017-08-20]
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