共 10 条
- [1] STRUCTURAL ASPECTS OF DO 31 JET-LIFT VTOL AIRCRAFT [J]. AERONAUTICAL JOURNAL, 1968, 72 (692): : 719 - &
- [2] FUEL OPTIMAL LANDING TRANSITIONS OF JET PROPELLED VTOL AIRCRAFT [J]. INGENIEUR ARCHIV, 1971, 40 (02): : 96 - &
- [3] FUEL MINIMAL TAKEOFF PATH OF JET LIFT VTOL AIRCRAFT [J]. JOURNAL OF AIRCRAFT, 1980, 17 (05): : 290 - 291
- [5] Analysis of conceptual parameters of lift-fan VTOL aircraft in transition [J]. Chang, M, 1600, Northwestern Polytechnical University (31):
- [6] EFFECTS OF INTRODUCING RESTORING MOMENT PROPORTIONAL TO STICK VELOCITY ON HOVERING OF AN UNSTABILISED JET-LIFT AIRCRAFT [J]. AERONAUTICAL QUARTERLY, 1964, 15 (01): : 53 - &
- [7] Optimal Flight Paths Reducing the Aircraft Noise during Landing [J]. MODELLING, COMPUTATION AND OPTIMIZATION IN INFORMATION SYSTEMS AND MANAGEMENT SCIENCES, PROCEEDINGS, 2008, 14 : 1 - 10
- [8] AERODYNAMIC INTERFERENCE EFFECTS WITH JET-LIFT V/STOL AIRCRAFT UNDER STATIC AND FORWARD-SPEED CONDITIONS [J]. ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1967, 15 (07): : 237 - &
- [10] Transition controller design of thrust-vectored vertical and/or short takeoff and landing aircraft based on single-step optimal method [J]. Zhu, Ji-Hong (jhzhu@tsinghua.edu.cn), 1600, Northeast University (35):