TsAGI Science Journal
Выходит 6 номеров в год
ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
SOLUTION OF THE INVERSE PROBLEM FOR AN AIRFOIL WITHIN THE FRAMEWORK OF THE REYNOLDS AVERAGED NAVIER-STOKES EQUATIONS
Том 44,
Выпуск 3, 2013,
pp. 371-385
DOI: 10.1615/TsAGISciJ.2013009695
Краткое описание
A new iterative method for solution of the inverse airfoil problem in a compressible gas flow within the framework of RANS equations has been developed. The method belongs to the class of residual correction methods. An airfoil geometry correction, decreasing the residual between the computed and desired pressure distributions, is defined by means of a correction block based upon the previously developed domestic inverse full-potential code. Several examples of inverse problem solution showing high efficiency of the method are given.
696 Просмотры статей
11 Загрузка статей
Метрики
Статьи с похожим содержанием:
Последний выпуск
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