Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane

Creator(s): Cahill, Jones F.
Creation Date: November 1944
Partner(s):
UNT Libraries Government Documents Department
Collection(s):
National Advisory Committee for Aeronautics Collection
Technical Report Archive and Image Library
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Total Uses: 1,513
Past 30 days: 42
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Date(s):
  • Creation: November 1944
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Serial Title: NACA Wartime Reports
Serial Title: NACA Memorandum Reports
Partner:
UNT Libraries Government Documents Department
Collection:
National Advisory Committee for Aeronautics Collection
Collection:
Technical Report Archive and Image Library
Identifier:
  • : 93R22091
  • URL: http://hdl.handle.net/2060/19930092801
  • REP-NO: NACA-WR-L-629
  • REP-NO: NACA-MR-L4K21
  • CASI: 19930092801
  • ARK: ark:/67531/metadc61411
Resource Type: Report
Format: Text
Rights:
Access: Public
Statement: No Copyright, Unclassified, Unlimited, Publicly available