俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
卷 40, 2009 册 4
DOI: 10.1615/TsAGISciJ.v40.i4
SEVERAL ASPECTS OF GAS FLOW WITH PRESCRIBED DISTRIBUTION OF HEAT SOURCES
pp. 401-417
DOI: 10.1615/TsAGISciJ.v40.i4.10
MONOTONIZATION OF THE FINITE ELEMENT METHOD IN THE PROBLEMS OF GAS DYNAMICS
pp. 419-436
DOI: 10.1615/TsAGISciJ.v40.i4.20
AERODYNAMIC CHARACTERISTICS OF MODELS OF VERTICAL TAKE-OFF AIRCRAFT (TILTROTOR) FOR A WIDE RANGE OF ANGLESOF ATTACK
pp. 437-452
DOI: 10.1615/TsAGISciJ.v40.i4.30
ANALYSIS OF THE SONIC BOOM INTENSITY USING NEAR-FIELD PERTURBATION UNDER THE AIRCRAFT, CALCULATED BY MEANS OF THE NONLINEAR THEORY
pp. 459-473
DOI: 10.1615/TsAGISciJ.v40.i4.50
NUMERIC INVESTIGATION OF THE VENTILATION SYSTEM OF AN ADVANCED AIRCRAFT PASSENGER CABIN
pp. 475-483
DOI: 10.1615/TsAGISciJ.v40.i4.60
A METHOD FOR TAKING INTO ACCOUNT THE INFLUENCE OF THE MODEL AND DYNAMOMETER WEIGHTS ON THE STRAIN-GAUGE BALANCE READINGS
pp. 485-495
DOI: 10.1615/TsAGISciJ.v40.i4.70
APPLICATION OF SIMILARITY TRANSFORMATION UPON PARAMETRIC INVESTIGATIONS OF FLUTTER
pp. 497-506
DOI: 10.1615/TsAGISciJ.v40.i4.80
AN ENGINEERING METHOD FOR DETERMINING CHARACTERISTICS OF A PROTECTIVE SCREEN AT IMPACT OF A NONLOCALIZED ENGINE FRAGMENT
pp. 507-516
DOI: 10.1615/TsAGISciJ.v40.i4.90
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INDEX, VOLUME 51, 2020