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TsAGI Science Journal

ISSN Print: 1948-2590
ISSN Online: 1948-2604

TsAGI Science Journal

Forthcoming Articles:

SELF-SIMILAR SOLUTIONS FOR VISCOUS COMPRESSIBLE GAS FLOW INSIDE A CONE
Murad Abramovich Brutyan , Umar Garunovich Ibragimov
DOI: 10.1615/TsAGISciJ.2018027158
THE INFLUENCE OF THE WINGTIP ON AIRFLOW PAST A WING
Olga V. Pavlenko , Alexander M. Razdobarin, Gennady A. Fedorenko
DOI: 10.1615/TsAGISciJ.2018027122
ACTIVE FLUTTER SUPPRESSION OF A HIGH ASPECT RATIO WING AIRCRAFT
Oktai. S. Mamedov, Sergey E. Paryshev , Valery N. Popovsky, Vsevolod I. Smyslov
DOI: 10.1615/TsAGISciJ.2018027114
DESIGN OF CONTROL SYSTEM ALGORITHMS FOR UNMANNED TILTROTOR
Andrei Georgievich Bushgens, Aleksandr Yurievich Voronin, Viktor Mikhailovich Kuvshinov, Veniamin Aleksandrovich Leontiev
DOI: 10.1615/TsAGISciJ.2018027091
VOLUME-CENTERED DISCHARGE IN SUPERSONIC AIR FLOW AT CONCENTRATED PROPANE AND OXYGEN INJECTION TO THE DISCHARGE ZONE
Vyacheslav Konstantinovich Alatortsev, Sergei Ivanovich Inshakov, Ivan Sergeevich Inshakov, Alexander Fedorovich Rozhkov, Vladimir Vladimirovich Skvortsov, Andrei Yur’evich Urusov, Alexander Alexandrovich Uspenskii
DOI: 10.1615/TsAGISciJ.2018027083
ON THE ASYMPTOTIC THEORY OF INTERACTION OF THE RUNNING PRESSURE PERTURBATION WITH THE BOUNDARY LAYER IN A SUPERSONIC FLOW
Vladimir Viktorovich Bogolepov, Vladimir Yakovlevich Neyland
DOI: 10.1615/TsAGISciJ.2018027076
DETERMINATION OF THE ADMISSIBLE RANGE LIMITS FOR MOUNTING THE SENSORS OF THE AIR SIGNAL SYSTEM
Nikolay Alekseevich Zlenko
DOI: 10.1615/TsAGISciJ.2018027046
EMPIRICAL-MATHEMATICAL MODELS IN THE PROBLEM OF OPTIMAL DESIGN OF THE SUSPENSION UNIT OF THE ENGINE NACELLE UNDER THE AIRCRAFT WING
Nikolai Alekseevich Zlenko, Evgenii Sergeevich Matyash, Sergey Vladimirovich Mikhaylov, Andrey Aleksandrovich Savelyev
DOI: 10.1615/TsAGISciJ.2018027031
SHOCK WAVE INTERACTION NEAR A CYLINDER ALIGNED NORMAL TO A BLUNTED PLATE Part I. GAS FLOW AND HEAT TRANSFER ON A PLATE NEAR A CYLINDER
Volf Yakovlevich Borovoy, Vladimir Evgen’evich Mosharov, Vladimir Nikolaevich Radchenko, Arkadii Sergeevich Skuratov
DOI: 10.1615/TsAGISciJ.2018026924
METHOD OF SOLVING THE INVERSE PROBLEM FOR WING-FUSELAGE COMBINATION USING REYNOLDS-AVERAGED NAVIER STOKES EQUATIONS
Anatoliy Longenovich Bolsunovskiy , Nikolay Petrovich Buzoverya , Irina Anatol'evna Gubanova, Nikita Aleksandrovich Pushchin, Kirill Igorevich Cherniy
DOI: 10.1615/TsAGISciJ.2018026907
STRENGTH ESTIMATION OF METAL-COMPOSITE JOINTS WITH NUISMER CRITERION APPLICATION
Yanina Stefanovna Borovskya , Mariya Alexandrovna Glebova , Vyacheslav Ivanovich Grishin , Natalia Vyacheslavovna Guseva
DOI: 10.1615/TsAGISciJ.2018026893
AIR INTAKE IN THE TRANSIENT REGIME OF RAREFIED GAS FLOW
A.I. Erofeev
DOI: 10.1615/TsAGISciJ.2018026789
VERIFICATION OF A COMPUTATIONAL DYNAMIC MODEL OF A LAUNCH VEHICLE STRUCTURE
A.G. Bakhtin, V.A. Titov
DOI: 10.1615/TsAGISciJ.2018026788
NUMERICAL INVESTIGATION ON THE INTERACTION OF A PAIR OF HOT OFF-DESIGN SUPERSONIC JETS WITH A JET BLAST DEFLECTOR
L.A. Bendersky, D.A. Lyubimov, A.O. Chestnykh
DOI: 10.1615/TsAGISciJ.2018026782
ON THE COMPRESSIBLE COUETTE FLOW
V.N. Golubkin, G.B. Sizykh
DOI: 10.1615/TsAGISciJ.2018026781
INFLUENCE OF LATERAL CONTROL SYSTEM ON TRANSPORT AIRCRAFT SPIN
D.A. Alieva, M.E. Sidoryuk, A.N. Khrabrov
DOI: 10.1615/TsAGISciJ.2018026767
COMPARATIVE NOISE ESTIMATION METHOD FOR GAS TURBINE POWER PLANTS OF JET PLANES
V.G. Dmitriev, V.F. Samokhin
DOI: 10.1615/TsAGISciJ.2018026769