Accession Number : AD0005479


Title :   ON THE EFFECT OF THICKNESS ON THE DAMPING IN ROLL OF AIRFOILS AT SUPERSONIC SPEEDS


Corporate Author : ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD


Personal Author(s) : Martin, John C ; Gerber, Nathan


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/005479.pdf


Report Date : Jan 1953


Pagination or Media Count : 59


Descriptors :   *DAMPING , *SUPERSONIC AIRFOILS , *THICK WINGS , ROLL , THEORY


Subject Categories : Aerodynamics


Distribution Statement : APPROVED FOR PUBLIC RELEASE