Citation: Av. Bulygin et al., CONCEPTION AND SELECTION OF DESIGN PARAME TERS OF TRANSPORT SCREEN PLANE, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 6-8
Citation: Ms. Safariev, DEVELOPMENT OF PLATE ANALOGY FOR THE CALC ULATION OF THE STRENGTH OF BEARING SURFACES OF SCREEN PLANES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 14-19
Citation: Ai. Bogomolov et Pk. Semenov, SYSTEM OF SCREEN PLANE FLIGHT CONTROL WIT H ADAPTATION PROPERTIES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 20-26
Citation: Av. Nebylov et Mv. Naumenko, OPTIMIZATION PROBLEM FOR THE SYSTEM OF ST ABILIZATION OF SCREEN PLANEMOVEMENT ALTITUDE ABOVE THE DISTURBED SEA, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 27-30
Citation: Ga. Pogosov et Vm. Soldatkin, INFORMATION SUPPLY OF THE SYSTEM FOR THE PREVENTION OF SCREEN PLANE MOVEMENT CRITICAL MODES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 31-34
Citation: Lg. Romanenko, SYNTHESIS OF CONTROL-SYSTEM OF SCREEN PLA NE LENGTHWISE MOVEMENT WITHSEPARATE CONTROL, PITCHING ANGLE AND FLIGHT ALTITUDE, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 35-40
Citation: Vm. Soldatkin, PRINCIPLES OF THE DESIGNING OF INFORMATIO N-CONTROL SYSTEM OF SAFETY GUARANTEE FOR THE SCREEN PLANE MOVEMENT, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 48-53
Citation: An. Ilinskii et al., METHOD OF AERODYNAMIC DESIGNING OF WING P ROFILE OF SCREEN PLANES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 54-63
Citation: Vm. Romanov, METHOD FOR THE CALCULATION OF THE FLOW-AR OUND OF FINITE-SPAN WINGS BY THE IDEAL NONCONDENSABLE LIQUID FLOW NEAR SCREENS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 64-68
Authors:
DREGALIN AF
ALTUNIN VA
PAVLOV OY
YAGOFAROV OK
Citation: Af. Dregalin et al., STUDY OF THE POTENTIAL INTENSIFICATION OF HEAT-EXCHANGE AND SEDIMENTATION PREVENTION PROCESSES IN SCREEN PLANE ENERGETIC UNITS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 69-76
Citation: Ds. Kovner et Ty. Mozzhorina, STUDY OF HIGH-TEMPERATURE TURBINES IN THE SUPERSONIC AIRCRAFT SYSTEMS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 77-81
Authors:
GARIFULLIN MF
ENIKEEV RK
KREICHMAN VL
KUZNETSOV IA
Citation: Mf. Garifullin et al., MODELING OF DYNAMIC LOADING OF SCREEN PLA NES DURING THE FLIGHT ABOVETHE IRREGULAR SEA TIDES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 85-88
Citation: Yv. Petrov, EXPERIMENTAL METHODS FOR MODELING OF ELAS TICALLY ATTACHED LOADS PARAMETERS WHILE TESTING DYNAMICALLY SIMILAR AIRCRAFT MODELS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 89-91
Authors:
DMITRIEV YI
KRYUKOVA LK
SYROMYATNIKOVA IN
Citation: Yi. Dmitriev et al., METHODS AND MEANS OF DEVICE CONTROL OF PI LOT CONDITION IN THE SCREENPLANES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 92-95
Citation: Ai. Matyazh et Ei. Rusakovskii, SCREEN PLANE DESIGN STUDIED IN AERODYNAMI C TUBES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 96-100
Authors:
NAZAROV DV
MILEKHIN VN
MOTYLINSKII IP
SHTATNOV YA
Citation: Dv. Nazarov et al., STUDY OF COMBINED DIAGRAM OF AIR CUSHIONI NG FORMATION, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 101-103
Citation: On. Emin et Vi. Kuznetsov, POTENTIAL UTILIZATION OF DUPLEX TURBINES WITH TURNING GRIDS IN TJM, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1995, pp. 104-106
Citation: Bm. Perlov, DYNAMIC ANALYSIS OF FLEXIBLE COMMUNICATIO NS OF AIRCRAFT SERVICING SYSTEMS IN THE AIR, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1995, pp. 3-7
Citation: Vv. Kuzmin, SOLUTION OF GEOMETRICALLY NONLINEAR PROBL EMS TAKING INTO ACCOUNT ROTATING UNDER THE DEFORMATION LOADS FOR THE REINFORCED ROTATION SHELL, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1995, pp. 8-13
Citation: Va. Pavlov, PHENOMENON OF CATASTROPHIC CHANGE OF SHAP ES OF AIRCRAFT BEARING SURFACES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1995, pp. 14-19
Citation: Yv. Petrov, MODELING AND STUDY OF THE EFFECT OF PARAM ETERS OF PYLON FORCE UNITS ON AEROELASTIC VIBRATIONS OF AIRCRAFT WINGS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1995, pp. 20-22