Citation: Vm. Adrov, PRINCIPLE OF LOCAL EQUIVALENCE OF STRESS- STRAIN DUE TO THE ANALYSIS OF FATIGUE DURABILITY, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 10-13
Citation: Sv. Andreev et Aa. Kuzmin, MECHANICS OF THE DEFORMATION OF 3-LAYERED ANISOTROPIC SHELL ELEMENTS OF AIRCRAFT CONSTRUCTIONS WITH COMPLEX CONTOUR, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 14-18
Citation: Yp. Zhigalko et Av. Konyukhov, STRESS-STRAINED CONDITION OF THIN-WALL CONSTRUCTION ELEMENTS HEATED WITH LOCALIZED FLOWS OF RADIATIVE ENERGY, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 19-25
Citation: Lg. Romanenko, SELECTING THE WEIGHT COEFFICIENTS FOR INTEGRAL QUADRATIC ESTIMATES WHILE DETERMINING OPTIMAL CHARACTERISTICS OF POLYNOMIALS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 33-40
Citation: Ek. Nugmanov et Va. Ovchinnikov, SOLVING THE INTEGRAL-EQUATION OF A WING THEORY BY GALERKIN TECHNIQUE, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 47-50
Citation: Vg. Pavlov et Gd. Peshatov, DIGITAL STUDIES OF THE EFFECT OF CURVATURE AND RELATIVE THICKNESS OF A WING PROFILE ON LIFT COEFFICIENTS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 51-55
Citation: Vn. Matveev et al., EXPERIMENTAL-DETERMINATION OF THE EFFECT OF EXTENT FACTORS ON MICROTURBINE EFFICIENCY, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 65-69
Citation: Vi. Petrenko et Vl. Popov, DESIGNING THE SOLID-FUEL CONTROLLED ENGINE DEVICE WITH A THERMAL BLADE, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 70-74
Citation: Ya. Kirsanov, EFFECT OF INSTABILITY AND HETEROGENEITY OF TEMPERATURE-FIELDS IN A WALL ON THE TEMPERATURE OF HEAT-CARRIER FLOWS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 75-79
Citation: Vm. Soldatkin, FORMATION OF OPERATION RESTRICTIONS, WARNING SIGNALS AND CONTROL ALGORITHMS IN EMERGENCY SITUATIONS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 85-92
Citation: Ri. Adgamov et Ar. Abzalov, MODEL RESEARCH OF NODES AND HARDWARE OF AIRCRAFT GTE DURING DESIGNINGOF OPTIMAL TEST TECHNOLOGIES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 93-97
Citation: Av. Korobko, CALCULATION OF TRAPEZOIDAL PLATES (MEMBRANES, CROSS-SECTIONS) BY THE INTERPOLATION METHOD, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 103-107
Citation: Vp. Smolentsev et al., CALCULATION OF NON-PROFILED TOLLS FOR THE COMBINED TREATMENT OF PLASTIC MATERIALS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (2), 1997, pp. 111-113
Citation: Ps. Gimadiev et al., NUMERICAL AND EXPERIMENTAL-STUDY OF STRIP CROSS-LIKE PARACHUTES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1997, pp. 6-11
Citation: Sp. Rychkov, DISCRETE MODEL SYSTEMS FOR THE ANALYSIS O F TAKE-OFF-LAUNCH AIRCRAFT CONDITIONS, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1997, pp. 12-18
Citation: Va. Talyzin, OPTIMAL SYNTHESIS OF EXCESSIVENESS SYSTEM S USING ELEMENTS WITH 2 FAILURE TYPES, Izvestia vyssih ucebnyh zavedenij. Aviacionnaa tehnika, (1), 1997, pp. 19-27