Do 335 Airfoil

Discussion in 'Technical Requests' started by s.flying, Dec 8, 2014.

  1. s.flying

    s.flying New Member

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    Does anyone know what airfoil was used on Do 335 tail assembly (vertical/horizontal stabilizer)?

    I have information regarding the wing (NACA 23018-630/NACA 23012-635) but i'm not able to find the former.
     
  2. Crimea_River

    Crimea_River Well-Known Member

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    I checked over at the now-closed LEMB forum and was able to confirm the info you already have though there is nothing on the tail assembly. Reference is made to scale drawings here A. L. BENTLEY DRAWINGS | Products and there's a nice set of drawings for the Pfeil which might help you. A quick scan does not seem to show sections through the stabilizers but the vertical stab seems to be symmetrical and not of airfoil section. That may stand to reason given the push/pull engine layout but I'm not an expert in such things.
     
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  3. Snautzer01

    Snautzer01 Well-Known Member

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    Cross tail made of 2 components both NACA 23012.5. The tail set up of the Do335 came forth out of the patented project P.59-04 patent number 728044 given to Dornier.
     
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  4. s.flying

    s.flying New Member

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    Thank you, much appreciated.
     
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