TsAGI Science Journal
年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
INVESTIGATION OF THE EFFECT OF ELASTIC DEFORMATIONS OF THE WING MODEL OF A WIDE-BODY COMMERCIAL TRANSPORT AIRCRAFT ON ITS AERODYNAMIC CHARACTERISTICS
巻 49,
発行 7, 2018,
pp. 771-780
DOI: 10.1615/TsAGISciJ.2018029252
要約
Based on the numerical solutions of the Navier-Stokes equations, a calculation study of the influence of the wing deformation caused by the effect of the aerodynamic load on the characteristics of a model of a wide-body commercial transport aircraft was carried out. The calculated data were compared with the results of measurements performed in a wind tunnel. It is shown that the technique used provides good agreement with the results of experimental measurements.
851 記事の閲覧数
11 記事のダウンロード
記事の統計
類似内容の記事:
最新号
KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY
NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER
ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION
EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE
ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE
WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT
NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION
POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS
A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR
INDEX, VOLUME 51, 2020