Accession Number : ADB807290


Title :   Wind-Tunnel Tests of Ailerons at Various Speeds. 1 - Ailerons of 0.20 Airfoil Chord and Tube Contour with 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil


Descriptive Note : Wartime rept.


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA


Personal Author(s) : Letko, W ; Denaci, H G ; Freed, C


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/b807290.pdf


Report Date : Jun 1943


Pagination or Media Count : 46


Descriptors :   *AERODYNAMIC CONTROL SURFACES , AILERONS , AIRFOILS , WIND TUNNEL TESTS


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE