Accession Number : AD0784259
Title : A Study of the Damping Characteristics on Models of Supersonic Airlines at Supersonic Speeds,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Tyunin,N. N. ; Ushakov,M. V.
Report Date : 24 JUL 1974
Pagination or Media Count : 11
Abstract : The article presents the results of an experimental study of the damping moment coefficients of the configuration of supersonic airliner models with small wing aspect ratios in a supersonic wind tunnel. A comparison of experimental and calculated data is presented.
Descriptors : *Supersonic aircraft, *Damping, *Wind tunnel models, Supersonic characteristics, Wind tunnel tests, Aspect ratio, Test methods, USSR, Angle of attack, Translations
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE