共 15 条
- [1] Assessment of engineering-level codes for missile aerodynamic design and analysis Atmosph. Flight Mech. Conf., 1600,
- [3] Thermodynamic Analysis on Pressurization Characteristics of Continuously Rotating Detonation Combustor Tuijin Jishu/Journal of Propulsion Technology, 2018, 39 (05): : 1057 - 1066
- [4] A 3D numerical analysis on the improvement of aerodynamic characteristics of the aerotrain wing Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2011, 77 (779): : 1410 - 1419
- [5] SUPERSONIC STABILITY AND CONTROL CHARACTERISTICS OF A CRUCIFORM MISSILE MODEL WITH DELTA WINGS AND AFT TAIL FIN CONTROLS. NASA Technical Memorandum, 1979,
- [7] Analysis on flow characteristics and aerodynamic-force-induced vibration of supersonic rocket-sled Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2022, 40 (05): : 1080 - 1089
- [8] Analysis of Hydraulic Characteristics of Control Organs. Energomashinostroenie, 1979, (07): : 4 - 5
- [9] ANALYSIS OF DYNAMIC CHARACTERISTICS OF STEPPING MOTOR SYSTEM IN CONSIDERATION OF ELASTICITY OF ROTATING SHAFT. Electrical Engineering in Japan (English translation of Denki Gakkai Ronbunshi), 1984, 104 (02): : 82 - 86