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Prototypical Polish Airliner Design......
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<blockquote data-quote="Justo Miranda" data-source="post: 24952" data-attributes="member: 960"><p>Sure, Terry.</p><p>The fuselage cross sections are oval semi-monocoque and was built up of transverse U-section wings and longitudinal Z-section stringers and smooth "Alclad" sheet, as you can see in the attached picture.</p><p></p><p>I do not have any drawings on the airfoil designed by Jerzy Dabrowski but you may try to find them at </p><p>http://www.soton.ac.uk/~jps7/D8%20website/Aerofoils%20used%20by%20aircraft.htm</p><p></p><p>David Lednicer </p><p>Analytical Methods, Inc. </p><p>2133 152nd Ave NE </p><p>Redmond, WA 98052 </p><p>dave@amiwest.com </p><p></p><p>or try a reconstruction using the program at http://www.modelgeeks.com/Uwe/Forum.aspx/air/351/airfoils-ho-to-compute</p><p>http://www.aae.uiuc.edu/m-selig/ads/aircraft.html</p><p></p><p>If everything fails, you may use the Douglas DC-2 (NACA 2215) airfoil, being certain that you will not err much.</p><p></p><p>All the best,</p><p>Justo</p></blockquote><p></p>
[QUOTE="Justo Miranda, post: 24952, member: 960"] Sure, Terry. The fuselage cross sections are oval semi-monocoque and was built up of transverse U-section wings and longitudinal Z-section stringers and smooth "Alclad" sheet, as you can see in the attached picture. I do not have any drawings on the airfoil designed by Jerzy Dabrowski but you may try to find them at http://www.soton.ac.uk/~jps7/D8%20website/Aerofoils%20used%20by%20aircraft.htm David Lednicer Analytical Methods, Inc. 2133 152nd Ave NE Redmond, WA 98052 dave@amiwest.com or try a reconstruction using the program at http://www.modelgeeks.com/Uwe/Forum.aspx/air/351/airfoils-ho-to-compute http://www.aae.uiuc.edu/m-selig/ads/aircraft.html If everything fails, you may use the Douglas DC-2 (NACA 2215) airfoil, being certain that you will not err much. All the best, Justo [/QUOTE]
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Prototypical Polish Airliner Design......
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