共 50 条
- [43] AIRCRAFT THRUST VECTORING USING FLEXIBLE NONAXISYMMETRIC NOZZLES JOURNAL OF AIRCRAFT, 1994, 31 (04): : 984 - 986
- [50] THRUST VECTOR CALCULATION FOR SUPERSONIC NOZZLES WITH AN OBLIQUE EXIT ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1984, 8 (02): : 110 - 112